DE102023100265A1 - Mobile quantum computer system executing quantum algorithms to increase sensor performance and accelerate sensor data processing - Google Patents

Abstract

The document presented here proposes a mobile device with a quantum computing system QUSYS, which includes a quantum computer QC1, QC2, and with sensors SENS. The SENS sensors and, if applicable, devices that are connected to the mobile device via wired and/or wireless data connections transmit sensor data to the QUSYS quantum computer system, which executes one or more quantum algorithms which increase the performance of SENS sensors and/or which Accelerate processing of the data and sensor data from the SENS sensors and/or other data.

Description

The document presented here hereby takes priority over the German patent application DE 10 2021 112 917.6 from May 18, 2021 and DE 10 2022 105 465.9 from March 8th, 2022.

State of the art

The writing presented here, for example, refers to the writings DE 10 2020 007 977 B4 , DE 10 2020 125 189 A1 , DE 10 2020 101 784 B3 , DE 10 2020 007 977 B4 and to the book Steven Prawer (editor), Igor Aharonovich (editor), “Quantum Information Processing with Diamond: Principles and Applications”, Woodhead Publishing Series in Electronic and Optical Materials, Volume 63, Woodhead Publishing, May 8, 2014, ISBN- 10: 0857096567, ISBN-13: 978-0857096562, the contents of which, to the extent that the legal system of a state in which a subsequent internationalization of this application takes place allows this, are part of the disclosure of the document presented here.

All of these documents do not describe the structure of a SW stack for an NV center based quantum computer with quantum dots comprising NV centers and nuclear core quantum bits with core quantum dots comprising the atomic nuclei of magnetic moment isotopes.

The quantum dots in the document presented here couple preferentially by means of magnetic dipole-dipole interaction. The quantum dots of the document presented here also preferably couple with the core quantum dots of the document presented here by means of magnetic dipole-dipole interaction.

Field of invention

The invention is directed to a quantum computer with a quantum computer stack or to a quantum computer that includes parts of a quantum computer stack and to the quantum computer stack itself.

The state of the art refers to the patent family of the German patent application DE 10 2020 125 169 A1 is referenced here as an example.

Task

The proposal is therefore based on the task of specifying a solution for the procedures for processing a software stack of a quantum computer based on NV centers.

This task is solved by an independent claim. Further refinements are the subject of subclaims.

Solution to the task

1 shows the structure of a quantum computer stack for an NV center based quantum computer.

Nuclear quantum bits ( ¹³ C, ¹⁴ N, ¹⁵ N) in a diamond material form the Qbits of the quantum computer. NV centers as Ancilla quantum bits represent electronic quantum bits. The NV centers connect the nuclear quantum bits ( ¹³ C, ¹⁴ N, ¹⁵ N) of the quantum computer within a quantum ALU. The writing presented here refers to Scripture WO 2021 083 448 A1 , the disclosure content of which is a complete part of the document presented here. In this context, the document presented here also refers to the patent family of the German patent application as an example DE 10 2020 125 169 A1 , the disclosure content of which is part of the application submitted here. The NV centers are in the 1 symbolized by the N - for nitrogen - and the e for the electron configuration of the respective NV center. The e symbolizes the respective electron configuration of the respective NV centers in the diamond material. The nuclear and electronic quantum bits are part of the hardware and interact via other hardware elements, such as those in the property rights applications of the patent family of the German patent application DE 10 2020 125 169 A1 are described, with each other.

Quantum computers

This document describes based on the information in the DE 10 2020 101 784 B3 described technical teaching a quantum computer. The document presented here describes a quantum computer with exemplary optical readout. Alternatively or in addition, the document presented here describes a quantum computer with exemplary electrical readout. The quantum computer presented here is based on quantum dots. The quantum dots preferably comprise paramagnetic centers in a substrate. The substrate preferably comprises diamond. The paramagnetic centers preferably include NV centers and/or SiV centers and/or TR1 centers and/or ST1 centers. The paramagnetic centers particularly preferably include NV centers. The quantum computer presented here preferably has an optical device. According to the technical teaching of the document presented here, the optical device is primarily used to irradiate quantum dots and thus to irradiate the paramagnetic centers with pump radiation. Secondly, the optical device is preferably used to extract fluorescence radiation from the quantum dots in the form of the NV centers. The optical device is therefore preferably used to extract fluorescence radiation from paramagnetic centers. The optical device is therefore preferably used to extract fluorescence radiation from NV centers. An optical functional element of the device is therefore preferably a paramagnetic center in a crystal, in particular an NV center in a diamond crystal and/or a SiV center in a diamond crystal and/or TR1 center in a diamond crystal and/or ST1 center in one Diamond crystal and/or a G center in a silicon crystal or a paramagnetic center in a mixed crystal made of elements from main group IV of the periodic table. In this context, the document presented here refers to the German patent DE 10 2020 101 784 B3 , whose technical doctrine forms the entirety of this disclosure, to the extent permitted by the law of the state in which nationalization of an international application of the contents of the document presented here takes place.

Such a quantum computer preferably comprises one or more micro-integrated circuits for generating the radio frequency signals, the microwave signals, the direct voltages and drive currents and the control of the light source LED, which serves as a pump radiation source for resetting the quantum dots of the quantum bits of the relocateable quantum computer.

All of these components of the deployable quantum computer, including the said micro-integrated circuits, are preferably accommodated on the circuit carrier, which can therefore be designed to be particularly compact.

The document presented here discloses a quantum computer with a SW stack (software stack). A smartphone or a portable quantum computing system or a vehicle or an autonomous means of transport or a robot or an aircraft or a missile or a rocket or a satellite or a rummissile or a space station or a floating device or a ship or an underwater vehicle or an underwater floating device or a deployable weapon system or another mobile device may include, for example, such a deployable quantum computer with a SW stack. For the sake of simplicity, the document presented here preferably refers to all of these devices as vehicles. A drive unit for such systems can also include such a deployable quantum computer. Such a drive unit can be an electrostatic or electromagnetic motor or an internal combustion engine or a heat engine or a turbine or a jet engine or a hypersonic engine or a rocket engine or a plasma engine or an engine with a magnetic field for confining a plasma, such as from the Vasimir project known. (See for example: Franklin R. Chang Diaz, F. Wall y Baitty, Jared P. Squire, Richard H. Goulding, Edgar A. Bering, Roger D. Bengtson, “The Vasimr Engine: Project Status and Recent Accomplishments,” downloadable on January 9, 2022 by
https://ntrs.nasa.gov/api/citations/20110011201/downloads/20110011201.pdf.) In the sense of the document presented here, deployability means that the claimed device is suitable and designed to move from a first location in a short time to be moved to a second location and to be operated both at the first location and at the second location and/or during the movement from the first location to the second location. Here, short time is typically a time shorter than a day, better shorter than 12 hours, better shorter than 6 hours, better shorter than 2 hours, better than 1 hour, better shorter than 30 minutes, better shorter than 15 minutes, better shorter than 5 minutes, better shorter than 2 minutes, better understood as shorter than 1 minute. The time for moving the device from a first location to a second location can also be 0s if the device is ready for use almost immediately from the user's perspective and/or is permanently ready for use and, for example, simply moves, i.e. remains usable, for example, during the movement. Readiness for use in the sense of the document presented here means being ready for intended use.

The following statements refer to the 1 .

The paper presented here proposes a deployable quantum computer QC in a mobile device. The deployable quantum computer QC has a software stack 1 (see 5 ) on. How the document presented here understands the term mobile device is described above. The core of the quantum computer QC forms a substrate D. The substrate D preferably has one or more quantum dots NV1, NV2, NV3. Their nature will be explained in more detail below. In this context, the document presented here also expressly refers to Scripture DE 10 2020 007 977 B4 , the content of which is a full part of the disclosure content of the document presented here, insofar as the legal system of the state in which the nationalization takes place allows this in the event of a later nationalization of a later international application.

The quantum dots NV1, NV2, NV3 are preferably located in the substrate D. The substrate D is preferably doped in the area of the quantum dots NV1, NV2, NV3. This doping preferably shifts the Fermi level in the area of the quantum dots NV1, NV2, NV3 in such a way that the quantum dots NV1, NV2, NV3 are electrically charged. The substrate D is preferably n-doped in the area of the quantum dots NV1, NV2, NV3. This n-doping preferably shifts the Fermi level in the area of the quantum dots NV1, NV2, NV3 in such a way that the quantum dots NV1, NV2, NV3 are negatively electrically charged.

Furthermore, the deployable quantum computer QC presented here preferably includes a light source LD and an associated light source driver LDRV. In order to be able to influence the quantum state of the quantum dots NV1, NV2, NV3 within the substrate D, the proposed deployable quantum computer QC preferably has one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 on. The deployable quantum computer QC preferably comprises a control device μC.

The control device µC preferably executes the software stack 1.

The control device µC executes an SPc laser control program 13. The control device μC preferably controls the light source driver LDRV and thus the emission of pump radiation LB with the pump radiation wavelength λ _pmp using the SPc laser control program 13. The proposed quantum computer QC preferably comprises a waveform generator WFG for controlling the light source driver LDRV by means of a transmission signal S5. The control device µC preferably also controls the waveform generator WFG using this SPc laser control program 13.

The control device μC executes a control program 15 for controlling the generation of an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3. Using this control program 15, the control device μC preferably also controls one or more and/or all devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3. The devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 change the quantum states of the quantum dots NV1, NV2, NV3 and/or one or more nuclear ones by means of control lines LV1, LV2, LH1 Core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The control device μC can preferably be used by means of this control program 15 and by means of the devices mWA, MW/RF-AWFG to generate an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 by controlling the control lines LV1, LV2, LH1 quantum dots NV1, NV2, Couple NV3 with core quantum dots of core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

The proposed quantum computer QC preferably also includes an optical system OS for irradiating the quantum dots NV1, NV2, NV3 in the substrate D with the pump radiation LB from the light source LD. The control device µC executes a control program 16 for controlling the optical system OS.

1. 1. ein oder mehrere Anwendungsprogramme 2 und/oder
2. 2. hybride quantentechnologisch/klassische Programme und Software 3 und/oder
3. 3. klassische Algorithmen 4, wobei klassische Algorithmen sind alle Algorithmen im Sinne dieses Dokuments, die keine Quantenzustände ändern, wenn sie durch die Steuervorrichtung µC ausgeführt werden, und/oder
4. 4. klassische Programme und Software 5, wobei klassische Programme und Software Programme im Sinne dieses Dokuments sind, die auf klassischen Rechnern 6 in Harvard- und von-Neumann-Architektur ablauffähig sind, und/oder
5. 5. quantentechnologische Algorithmen 7, wobei quantentechnologische Algorithmen im Sinne dieses Dokuments zumindest einen Quantenzustand zumindest eines Quantenbits, das zumindest einen Quantenpunkt NV1, NV2, NV3 des Quantencomputers QC und/oder zumindest einen Kernquantenzustand zumindest eines Kernquantenbits, das zumindest einen Quantenpunkt CI1₁, CI1₂, CI1₃, CI2₁, CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ des Quantencomputers QC aufweist, ändern, wenn die Steuervorrichtung µC diese quantentechnologischen Algorithmen ausführt, und/oder
6. 6. abstrakte Quantengatter-Modelle 8 und/oder
7. 7. einen Transcompiler 9 , bevorzugt mit Optimierer- und Quantenfehlerkorrekturfunktion, und/oder
8. 8. ein Quantengatter-Hardware-Modell 11 und/oder
9. 9. das Kontrollprogramm 12 für die Kontrolle und Steuerung des einen oder der mehreren Mikrowellen- und/oder Radiowellenfrequenzgeneratoren MW/RF-AWFG zur Erzeugung eines elektromagnetischen Wellenfeldes mittels einer oder mehrerer Mikrowellen- und/oder Radiowellenantenne mWA, insbesondere vertikaler Leitungen LV1, LV2 oder horizontaler Leitungen LH1 am jeweiligen Ort der Quantenpunkte NV1, NV2, NV3, zum Einwirken auf die Quantenpunkte NV1, NV2, NV3 des Quantencomputers QC und/oder der Quantenzustände der Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁, CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ des Quantencomputers QC, und/oder
10. 10. ein SPc Laser-Kontrollprogramm 13 für die Kontrolle und Steuerung des Wellenformgenerators WFG und des Lichtquellentreibers LDRV und damit der Lichtquelle LD, die mittels der Pumpstrahlung LB der Lichtquelle LD auf die Quantenpunkte NV1, NV2, NV3 des Quantencomputers QC einwirkt, und/oder
11. 11. ein Kontrollprogramm 14 für die Ansteuerung die Kontrolle und das Auslesen von Werten der Mittel PD, V zum optischen Auslesen der Quantenpunkte NV1, NV2, NV3 des Quantencomputers QC und/oder der Quantenzustände der Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁, CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ des Quantencomputers QC durch die Steuervorrichtung µC und/oder
12. 12. ein Kontrollprogramm 16 zur Kontrolle und Steuerung des optischen Systems OS, um das Einstrahlen des Laser-Strahls LB in das Substrat D bei Bedarf zu optimieren, und/oder
13. 13. ein Kontrollprogramm 17 für die Ausführung durch die Steuervorrichtung µC und zur Kontrolle und Einstellung von DC-Strompegeln und/oder DC-Spannungspegeln zu Beeinflussung von bestimmten Quantenpunkten NV1, NV2, NV3 des Quantencomputers QC und/oder bestimmten Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁, CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ des Quantencomputers QC in der Art, dass sie ggf. nicht an einer Hardware-Operation teilnehmen oder an einer Hardware-Operation teilnehmen, und/oder
14. 14. ein Positionskontrollprogramm 22 zur Kontrolle und Steuerung einer Positioniervorrichtung XT, YT zur Positionierung und ggf. Ausrichtung des Substrats D gegenüber dem optischen System OS und/oder
15. 15. ein Temperaturkontrollprogramm 23 zur Erfassung der Temperatur mittel Temperatursensoren ST und zur Regelung einer Temperatur auf eine Zieltemperatur und zur Kontrolle einer oder mehrerer Kühlvorrichtungen KV und/oder einer oder mehrerer Closed Loop Helium Gas Cooling-Systeme HeCLCS und
16. 16. ein Datenschnittstellenprogramm 28 zur Steuerung und Kontrolle einer oder mehrerer Datenschnittstellen DBIF und/oder
17. 17. ggf. ein Fahrzeugkontrollprogramm 24 zur Kontrolle und Steuerung von ggf. vorhandenen Fahrzeugfunktionen eines ggf. fahrenden, verlegbaren Quantencomputers QC und/oder
18. 18. ein oder mehrere Messwerterfassungsprogramme 26 zur Abfrage der Messwerte und zur Steuerung und Kontrolle der zugehörigen Messsysteme und
19. 19. ein Kryptografieprogramm 25 zur Verschlüsselung und/oder Entschlüsselung von Daten, die der Quantencomputer QC und/oder die Steuervorrichtung µC über die die Datenschnittstelle DBIF erhalten, und/oder zur Verschlüsselung und/oder Entschlüsselung von anderen Daten des Quantencomputers QC, und/oder
20. 20. ggf. eine Fahrzeugzustandsermittlungsprogramm 27 zur Lagebeurteilung des Gesamtzustands des Fahrzeugs und/oder der Umgebung des Fahrzeugs in Abhängigkeit von Messwerten.

The control device µC preferably has a memory one or more RAM, NVM. the control device µC for program commands and data. The memory content of this memory RAM, NVM. the control device preferably includes µC

1. 1. one or more application programs 2 and/or
2. 2. hybrid quantum technology/classical programs and software 3 and/or
3. 3. classical algorithms 4, where classical algorithms are all algorithms in the sense of this document that do not change quantum states when they are executed by the control device µC, and / or
4. 4. classic programs and software 5, whereby classic programs and software are programs in the sense of this document that can run on classic computers 6 in Harvard and von Neumann architecture, and/or
5. 5. quantum technological algorithms 7, wherein quantum technological algorithms in the sense of this document have at least one quantum state of at least one quantum bit, which has at least one quantum dot NV1, NV2, NV3 of the quantum computer QC and/or at least one core quantum state of at least one core quantum bit, which has at least one quantum dot CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC, change when the control device µC executes these quantum technological algorithms, and/or
6. 6. abstract quantum gate models 8 and/or
7. 7. a transcompiler 9, preferably with an optimizer and quantum error correction function, and/or
8. 8. a quantum gate hardware model 11 and/or
9. 9. the control program 12 for the control and control of the one or more microwave and / or radio wave frequency generators MW / RF-AWFG for generating an electromagnetic wave field by means of one or more microwave and / or radio wave antenna mWA, in particular vertical lines LV1, LV2 or horizontal lines LH1 at the respective location of the quantum dots NV1, NV2, NV3, for influencing the quantum dots NV1, NV2, NV3 of the quantum computer QC and / or the quantum states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC, and/or
10. 10. an SPc laser control program 13 for the control and control of the waveform generator WFG and the light source driver LDRV and thus the light source LD, which acts on the quantum dots NV1, NV2, NV3 of the quantum computer QC by means of the pump radiation LB of the light source LD, and / or
11. 11. a control program 14 for controlling and reading out values of the means PD, V for optically reading out the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC by the control device µC and/or
12. 12. a control program 16 for monitoring and controlling the optical system OS in order to optimize the irradiation of the laser beam LB into the substrate D if necessary, and / or
13. 13. a control program 17 for execution by the control device µC and for controlling and setting DC current levels and/or DC voltage levels to influence specific quantum points NV1, NV2, NV3 of the quantum computer QC and/or specific core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC in such a way that they may not participate in a hardware operation or participate in a hardware operation, and/or
14. 14. a position control program 22 for checking and controlling a positioning device XT, YT for positioning and, if necessary, aligning the substrate D with respect to the optical system OS and/or
15. 15. a temperature control program 23 for detecting the temperature using temperature sensors ST and for regulating a temperature to a target temperature and for controlling one or more cooling devices KV and / or one or more closed loop helium gas cooling systems HeCLCS and
16. 16. a data interface program 28 for controlling and monitoring one or more data interfaces DBIF and/or
17. 17. if necessary, a vehicle control program 24 for checking and controlling any existing vehicle functions of a possibly moving, deployable quantum computer QC and/or
18. 18. one or more measured value acquisition programs 26 for querying the measured values and for controlling and monitoring the associated measuring systems and
19. 19. a cryptography program 25 for encrypting and/or decrypting data that the quantum computer QC and/or the control device µC receives via the data interface DBIF, and/or for encrypting and/or decrypting other data of the quantum computer QC, and/or
20. 20. If necessary, a vehicle condition determination program 27 for assessing the situation of the overall condition of the vehicle and/or the surroundings of the vehicle depending on measured values.

Furthermore, the proposed deployable quantum computer QC preferably comprises an optical and/or electronic quantum state readout device for reading out the current quantum states of the quantum dots NV1, NV2, NV3. In the case of an optical quantum state readout device, the quantum state readout device preferably comprises a photodetector PD and an amplifier V.

In the case of an electrical quantum state readout device, the quantum state readout device preferably comprises contacts for contacting the substrate D and a voltage source for generating an extraction voltage between such contacts of the substrate D and an amplifier V for amplifying the thus extracted photocurrent of the quantum dots NV1, NV2, NV3.

The amplifier V can include a transimpedance amplifier as an internal amplifier IVV. In this case, the quantum state reading device comprises a device for electronically reading out the states of the quantum dots NV1, NV2, NV3.

Typically, the waveform generator WFG generates a light source control signal S5, typically depending on settings of the control device µC. Typically, the SPc process influences and/or controls laser control program 13, which executes the control device µC, the light source control signal S5. The light source driver LDRV preferably supplies the light source LD with electrical energy. This supply of the light source LD with electrical energy preferably takes place a) depending on the light source control signal S5 and possibly typically b) depending on the settings of the control device µC and typically c) depending on the sequence of the SPc laser control program 13. The control device µC controls typically the waveform generator WFG depending on the sequence of the SPc laser control program 13.

The light source LD at least temporarily irradiates the quantum dot or the multiple quantum dots NV1, NV2, NV3 using the optical system OS with pump radiation LB of the pump radiation wavelength λ _pmp . The control device µC executes a control program 16 for controlling the optical system OS. As a result, the sequence of a control program 16 for controlling the optical system OS controls the at least temporary irradiation of the quantum dot or the multiple quantum dots NV1, NV2, NV3 with pump radiation LB of the pump radiation wavelength λ _pmp by the light source LD by means of the optical system OS.

The one or more quantum dots NV1, NV2, NV3 emit fluorescence radiation FL with a fluorescence radiation wavelength λ _fl as a result of the irradiation with electromagnetic radiation of the pump radiation wavelength λ _pmp .

In the case of optical reading of the quantum states of the quantum dots NV1, NV2, NV3, the photodetector PD detects at least part of the fluorescence radiation FL by means of the optical system OS. The control device µC then executes a control program 12 for controlling the system for optically reading out the quantum states of the quantum dots NV1, NV2, NV3. The system for optically reading out the quantum states of the quantum dots NV1, NV2, NV3 preferably comprises a photodetector PD and a subsequent amplifier V. In this case, the photodetector PD converts at least part of the fluorescence radiation FL into a receiver output signal S0. A subsequent amplifier V amplifies and, if necessary, filters the receiver output signal S0 into a received signal S1. The control device µC executes the control program 12 for controlling the photodetector PD and the amplifier V.

In the case of electronic reading of the quantum states of the quantum dots NV1, NV2, NV3, the device for electronically reading out the states of the quantum dots NV1, NV2, NV3 generates the received signal S1. The control device µC controls the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1 by means of the control program 15 for controlling the generation of an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 , NV2, NV3. The control program 15 for controlling the generation of an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 can be controlled by controlling one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2 , NV3 change. The SPc laser control program 13 for controlling the light source driver LDRV can change states of the quantum dots NV1, NV2, NV3 by controlling the emission of the light source LD. The control device µC can thus control the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or by controlling the emission of the light source LD states of the quantum dots NV1 , NV2, NV3 change. The control device µC can therefore also be used to control one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or by controlling the emission of the light source LD states of the Couple quantum dots NV1, NV2, NV3 with each other.

For this purpose, the control device μC typically has means for generating a measured value signal S4 with one or more measured values from one or more received signals S1. The measured value signal S4 depends on quantum states of quantum dots NV1, NV2, NV3.

What is special about the quantum computer QC is that, in contrast to the prior art, the deployable quantum computer QC and/or the mobile device has a deployable power supply (LDV, TS, BENG, SRG) for supplying at least some of the sub-devices of the quantum computer QC with energy.

The control device µC preferably controls this deployable energy supply (LDV, TS, BENG, SRG) using an energy supply control program. The energy supply control program is preferably a hardware program that the control device μC or another computer unit of the quantum computer QC continuously executes.

The relocatable energy supply (LDV, TS, BENG, SRG) preferably has a mobile energy supply (LDV, TS, BENG) and an energy processing device SRG, in particular a voltage converter or a voltage regulator or a current regulator.

A further embodiment of the deployable quantum computer QC preferably has not only quantum dots NV1, NV2, NV3, but also one or more nuclear core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . In this case, the proposed deployable quantum computer QC preferably also has one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the core quantum dots CI1 ₂ , CI1 ₃ , CI2 1 , _{CI2 2 ,} CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ on. Typically, the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are entirely or at least partially identical to the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3, which then at the same time also have one or more devices for generating an electromagnetic wave field at respective locations of the core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are. Preferably, the control program for controlling the generation of an electromagnetic wave field at the respective location of the core quantum points CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ is identical to the control program 15 for the control the generation of an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3. The control device μC preferably executes said control program for controlling the generation of an electromagnetic wave field at the respective location of the core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

The quantum dots NV1, NV2, NV3 and the nuclear core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are preferably located in the common substrate D.

The control device μC preferably controls the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field using the control program 15. The control device μC can then preferably by means of the control program 15 by controlling the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field and/or by controlling the emission of the light source LD can quantum states of the quantum dots NV1, NV2, NV3 and/or or change quantum states of the core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The control device μC can then preferably use the control program 15 by controlling one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field and/or by controlling the emission of the light source LD, quantum dots NV1, NV2, NV3 with other quantum dots NV1 , NV2, NV3 The control device µC can then preferably use the control program 15 by controlling one or more devices mWA, MW/RF-AWFG to generate an electromagnetic wave field and/or by controlling the emission of the light source LD, quantum dots NV1, NV2, Couple NV3 with core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ . The control device μC can then preferably be controlled by means of the control program 15 by controlling one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field and/or by means of the SPc laser control program 13 by controlling the emission of the light source LD core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ with other core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ pair. The measured value signal S4 depends on quantum states of quantum dots NV1, NV2, NV3 and/or on states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

The mobile energy supply (LDV, TS, BENG) preferably supplies the energy processing device SRG with energy, the energy processing device SRG in turn preferably supplying other device parts of the deployable quantum computer QC with electrical energy.

The mobile energy supply (LDV, TS, BENG) preferably includes a charging device LDV and a disconnecting device TS and an energy reserve BENG. This enables an improvement in the EMC sensitivity of the deployable quantum computer QC. (EMC = electromagnetic compatibility). For this purpose, the proposed deployable quantum computer QC preferably has a first operating mode and a second operating mode. In the first operating mode of the deployable quantum computer QC, the separating device TS first connects the charging device LDV with the energy reserve BENG, so that the charging device LDV charges the energy reserve BENG with electrical energy from an external energy supply PWR in this first operating mode. In the first operating mode, the separation device TS first connects the charging device LDV to the energy processing device SRG and secondly, the charging device LDV supplies the energy processing device SRG with electrical energy from the external energy supply PWR. In the second operating mode, firstly the separating device TS preferably separates the charging device LDV from the energy reserve BENG and secondly the separating device TS separates the charging device LDV from the energy processing device SRG. Thirdly, in the second operating mode, the energy reserve BENG preferably supplies the energy processing device SRG with electrical energy.

In a further embodiment, the deployable quantum computer QC includes a housing GH and a shield AS. Preferably there are the light source LD and the light source driver LDRV and the substrate D and the devices mWA, MW/RF-AWFG for generating the electromagnetic wave field and the control device µC and the memory RAM, NVM of the control device µC and the optical system OS and if necessary. the amplifier V and the shield AS are inside the housing GH. This protects these device parts and possibly the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 _{1 , CI2 2 ,} CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in the substrate D from disruptive EMC influences . Typically, the shield AS can be part of the housing GH or the housing GH itself. Preferably there are at least parts of the device parts of the energy supply (LDV, TS, BENG, SRG) of the deployable quantum computer QC or those parts of the energy supply (LDV, TS, BENG, SRG) of the deployable quantum computer QC that provide an autonomous energy supply for a certain time enable autonomous operation of the deployable quantum computer QC, located within the common housing GH. The parts preferably have their own shielding AS.

An energy processing device SRG and an energy reserve BENG of the energy supply (LDV, TS, BENG, SRG) of the quantum computer QC are preferably located within the shield AS.

So that the relocatable quantum computer QC can be operated as a mobile quantum computer QC even during relocation, the relocatable quantum computer QC includes means for its operation, the relocatable quantum computer QC and all the necessary means for operating this relocatable quantum computer QC being part of a mobile device. To make this possible, these means for operating the deployable quantum computer QC are typically also deployable. For the same reason, these means for operating the deployable quantum computer QC are preferably part of the deployable quantum computer QC. Both the deployable quantum computer QC and these means for operating the deployable quantum computer QC are preferably part of the mobile device. It is typically irrelevant whether the operation of the deployable quantum computer QC is coupled to means and/or commands from outside the deployable quantum computer QC despite the presence of all means for operating the deployable quantum computer QC as part of the deployable quantum computer QC.

As already mentioned above, the deployable quantum computer QC is often part of a mobile device, the mobile device in particular being a smartphone or a portable quantum computer system or a vehicle or a robot or an aircraft or a missile or a satellite or a rum missile or a space station or a Floating body or a ship or an underwater vehicle or an underwater floating body or a deployable weapon system or another mobile device.

The deployable quantum computer QC preferably comprises a positioning device XT, YT. The control device µC preferably executes a position control program 22 for checking and controlling the positioning device XT, YT. The position control program 22 for checking and controlling the positioning device XT, YT can preferably position the substrate D relative to the optical system OS by means of the positioning device XT, YT in such a way that the optical system OS works in cooperation with the one or more devices mWA, MW/RF -AWFG for generating an electromagnetic wave field, firstly in a first positioning a first set of quantum dots with a first number of quantum dots and possibly a second number of core quantum dots and secondly in a second positioning a second set of quantum dots with a third number of quantum dots and possibly a fourth number of core quantum dots. The control device μC preferably controls the positioning device XT, YT for the substrate D by means of the position control program 22 in such a way that it assumes the first positioning or the second positioning or further positioning. In this way, the deployable quantum computer QC can always reconfigure itself depending on its operating temperature during operation and/or during breaks in operation so that it can always use a maximum of quantum dots and core quantum dots.

In a further refinement, the deployable quantum computer QC therefore has a temperature sensor ST, which provides a temperature measurement value for the temperature of the substrate D or for the temperature of a part thermally connected to it Device of the deployable quantum computer QC determined. The control device µC preferably evaluates the temperature measurement values of the temperature sensor ST. The position control program 22, which executes the control device μC to monitor and control a positioning device XT, YT, preferably uses the temperature measurement values of the temperature sensor ST.

This results in a version of the deployable quantum computer QC, wherein the deployable quantum computer QC is set up and intended to work with a reduced first number of quantum dots even at room temperature of the substrate D or a temperature measurement value that corresponds to a value greater than 0 ° C can. At the same time, however, the deployable quantum computer QC is also set up and intended to be able to work with an increased, third number of quantum dots at a temperature measurement value that corresponds to a value less than 0 ° C. In this way, the deployable quantum computer QC can always reconfigure itself depending on its operating temperature during operation and/or during breaks in operation so that it can always use a maximum of quantum dots and core quantum dots.

The document presented here therefore discloses in one form a deployable quantum computer QC, which is set up and intended to work with a reduced second number of core quantum dots even at room temperature of the substrate D or a temperature measurement value that corresponds to a value greater than 0 ° C can. Preferably, the deployable quantum computer QC is simultaneously set up and intended to be able to work with an increased fourth number of core quantum dots at a temperature measurement value that corresponds to a value less than 0 ° C. In this way, the deployable quantum computer QC can always reconfigure itself depending on its operating temperature during operation and/or during breaks in operation so that it can always use a maximum of quantum dots and core quantum dots.

In a further embodiment, the deployable quantum computer QC has one or more deployable cooling devices KV, which can be deployed together with the deployable quantum computer (QC). One or more of the deployable cooling devices KV are preferably suitable and/or intended to control the spin temperature of quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or to lower the temperature of the substrate D. The control device μC preferably controls one or more relocateable cooling devices KV by means of a temperature control program 23. The control device µC preferably controls one or more deployable cooling devices KV by means of a temperature control program 23 depending on a temperature measurement value from a temperature sensor ST. The control device μC can, for example, use the temperature control program 23 to emulate a PID controller or a PD controller or a PI controller or another controller with a more complex control characteristic or the like.

In a further embodiment, one or more such cooling devices KV lower the temperature of quantum dots NV1, NV2, NV3 and/or the temperature of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or the temperature of the substrate D to such an extent that the deployable quantum computer QC can work with a third number of quantum dots NV1, NV2, NV3 that is increased compared to the reduced first number of quantum dots NV1, NV2, NV3. One or more such cooling devices KV preferably lower the temperature of quantum dots NV1, NV2, NV3 and/or the temperature of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or the temperature of the substrate D to such an extent that the quantum computer QC has a reduced second number of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ an increased fourth number of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ can work.

In a further embodiment, one or more of the relocatable cooling devices KV of the quantum computer QC include one or more closed loop helium gas cooling systems HeCLCS or one or more relocatable closed loop helium gas cooling systems HeCLCS include one or more relocatable cooling devices KV.

In a further embodiment, the deployable quantum computer QC includes a deployable second deployable energy supply BENG2, which is different from the first deployable energy supply BENG. The second relocatable energy supply BENG2 preferably supplies one or more of the relocatable cooling devices KV and/or one or more of the closed loop helium gas cooling systems HeCLCS with energy.

In another embodiment, the deployable quantum computer QC and/or the mobile device have a mobile data interface DBIF, in particular a mobile radio data interface and/or a wired data interface. The control device µC preferably controls and controls this data interface DBIF by means of a data interface program 28.

Preferably, by means of this data interface DBIF, in a further embodiment, a higher-level computer system, for example a central control device ZSE, can control the control device µC in such a way that the control device µC of the deployable quantum computer QC can use the deployable quantum computer QC to carry out at least one manipulation of a state of at least one quantum bit of the quantum bits NV1, NV2, NV3 and/or to carry out at least one manipulation of a state of at least one nuclear core quantum bit of the nuclear core quantum bits CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The higher-level central control unit ZSE preferably controls the control device μC via the mobile data interface DBIF and the data interface program 28.

The first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 preferably comprise one or more batteries and/or one or more accumulators or one or more capacitors and/or one or more interconnection of several of these energy storage devices. The deployable quantum computer QC and/or the mobile device preferably have one or more charging devices LDV. Typically, one or more charging devices LDV are intended and/or are intended to store energy at least temporarily in at least some or all of the rechargeable energy storage devices BENG, BENG2.

In a variant, in the deployable quantum computer QC, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 can comprise one or more energy stores that generate energy from at least one or more fluids by means of chemical and/or electrochemical processes. In this case, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 and/or the quantum computer QC preferably have one or more storage tanks for these fluids. One or more of these storage tanks supply one or more energy storage devices of the quantum computer QC with one or more of these fluids, which typically serve to generate energy. Preferably, one or more of the energy storage devices include one or more galvanic cells and/or one or more fuel cells and/or one or more internal combustion engines and/or turbines and the like, each of which is coupled to one or more electrical generators, and/or one or a plurality of thermal energy conversion machines, each coupled to one or more electrical generators. One or more of the mobile energy supplies of the quantum computer QC preferably have one or more energy processing devices SRG, in particular one or more voltage converters and/or one or more voltage regulators and/or one or more current regulators. One or more of the energy storage devices preferably supply the energy processing devices SRG with energy. One or more of the energy processing devices SRG preferably in turn supply one or more device parts of the quantum computer QC with electrical energy that has been suitably prepared and stabilized for the relevant device part.

In a further variant of the deployable quantum computer QC, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise one or more energy stores that generate energy using mechanical processes. One or more of these energy stores then preferably comprise one or more generators and/or one or more alternators and/or one or more electric motors that can be operated as a generator. Typically, one or more mobile energy supplies of the quantum computer QC have one or more energy processing devices SRG, in particular one or more voltage converters or one or more voltage regulators or one or more current regulators. One or more of the energy storage devices supply one or more of the energy processing devices SRG with energy. One or more of the energy processing devices SRG then preferably supply one or more other device parts of the deployable quantum computer QC with electrical energy.

In a further variant of the deployable quantum computer QC, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 preferably comprise one or more energy storage devices that generate energy by converting electromagnetic radiation, in particular light, into electrical energy. For this purpose, one or more of the energy storage devices preferably include one or more solar cells and/or one or more functionally equivalent devices, such as PN junctions. In this case, one or more of the mobile energy supplies of the quantum computer QC preferably have one or more energy processing devices SRG, in particular one or more voltage converters and/or one or more voltage regulators and/or one or more current regulators. One or more of the energy stores of the energy reserve BENG, BENG2 of the quantum computer QC then typically supply one or more of the energy processing devices SRG with energy at least temporarily gie. One or more energy processing devices SRG then supply one or more other device parts of the quantum computer QC with electrical energy.

In a further variant of the deployable quantum computer QC, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise one or more energy storage devices that generate energy using nuclear processes. One or more of the mobile energy supplies of the quantum computer QC include one or more energy processing devices SRG, in particular one or more voltage converters and/or one or more voltage regulators and/or one or more current regulators. One or more of the energy stores of the energy reserve BENG, BENG2 of the quantum computer QC preferably supply one or more of the energy processing devices SRG with energy at least temporarily. One or more of these energy processing devices SRG then in turn supply one or more device parts of the deployable quantum computer QC with electrical energy.

In a further embodiment, one or more of the energy storage devices comprise one or more thermonuclear batteries or radionuclide batteries or one or more devices that are functionally equivalent to such a thermonuclear battery.

In a further variant, the substrate D comprises diamond. In this case, one or more of the quantum dots NV1, NV2, NV3 in the substrate D are preferably defect centers and/or paramagnetic centers in diamond. One or more of the defect centers in diamond NV centers or ST1 centers or SiV centers or TR12 centers are then particularly preferred.

The deployable quantum computer QC preferably comprises one or more core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ based on isotopes with a magnetic moment μ. The core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ are preferably coupled to quantum dots NV1, NV2, NV3.

Preferably, the substrate D is essentially isotopically pure, at least in regions in the area of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and the quantum dots NV1, NV2, NV3. This has the advantage that the magnetic moments of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and the quantum dots NV1, NV2, NV3 do not have such parasitic magnetic moments of impurities in the substrate D. For this purpose, the isotopes of the substrate D, apart from atoms that form the core quantum dots CI11, CI12, CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ , preferably have essentially no magnetic nuclear moment.

In a further embodiment, the deployable quantum computer QC has one or more fans and/or one or more heat exchangers for heat exchange with the environment and/or one or more heat exchangers for heat exchange with the ambient air and/or one or more radiation coolers for heat exchange with the ambient air or the environment by means of electromagnetic heat radiation. The control device µC preferably controls and monitors the one or more fans and/or the one or more heat exchangers by means of the temperature control program 23, which the control device µC executes.

In a further variant of the deployable quantum computer QC, one or more of the fans and/or one or more of the heat exchangers exchange energy in the form of heat with one or more of the deployable cooling devices KV.

In a further modification, the deployable quantum computer QC has an internal shielding AS. The internal shielding AS preferably shields the substrate D with the quantum dots NV1, NV2, NV3 and possibly the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ against electromagnetic Fields of the control device µC and / or the memory RAM, NVM and / or the power supply SRG, TS, LDV, BENG, BENG2 and / or the light source driver LDRV and / or the light source LD. In a further modification, the deployable quantum computer QC has an internal shielding AS. The internal shielding AS preferably shields the substrate D with the quantum dots NV1, NV2, NV3 and possibly the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ against magnetic fields the control device µC and/or the memory RAM, NVM and/or the power supply SRG, TS, LDV, BENG, BENG2 and/or the light source driver LDRV and/or the light source LD.

In order to be able to relocate the relocatable quantum computer QC, the relocatable quantum computer QC is in this case preferably equipped, at least temporarily, with one or more wheels or a chassis or functionally equivalent device parts, which can also be driven and / or braked.

In another form, the deployable quantum computer has QC, at least temporarily one or more drive devices. According to the proposal, one or more of the drive devices is a wheel or a propeller or a propeller or a turbine or a rocket engine or a drive wheel or an MHD engine. MHD stands for magnetohydrodynamic. In this case, the control device μC can, for example, execute a vehicle control program 24 that controls and controls the vehicle functions of such a deployable quantum computer QC. The control device μC of the quantum computer QC can, for example, access vehicle functions such as drive control, brakes, navigation devices and the like and thus control the vehicle if necessary.

In embodiments of the deployable quantum computer QC, which are to be operated in a fluid and moved for deployment, it is expedient if, in certain applications, such a deployable quantum computer QC has aerodynamically and/or hydrodynamically shaped functional elements for reducing and/or controlling aerodynamic effects and/or hydrodynamic Effects and / or for generating dynamic buoyancy, in particular wings and / or flaps.

• - die Steuervorrichtung µC und/oder
• - der Speicher RAM, NVM der Steuervorrichtung µC und/oder
• - der Rechnerkern CPU und/oder
• - die Datenschnittstelle DBIF und/oder
• - die interne Datenschnittstelle MDBIF und/oder
• - der Lichtquellentreiber LDRV und/oder
• - der Wellenformgenerator WFG und/oder
• - der Verstärker V und/oder
• - der Fotodetektor PD und/oder
• - die erste Kameraschnittstelle CIF und/oder
• - die zweite Kameraschnittstelle ClF2 und/oder
• - die erste Kamera CM1 und/oder
• - die zweite Kamera CM2 und/oder
• - der Temperatursensor ST und/oder
• - der Mikrowellen- und/oder Radiowellenfrequenzgenerator MW/RF-AWFG zur Erzeugung weitestgehend frei vorgebbarer Wellenformen und/oder
• - die Magnetfeldsensoren MSx, MSy, MSz und /oder
• - die Magnetfeldsteuerungen MFSx, MFSy, MFSz und/oder
• - die erste Energieaufbereitungsvorrichtung SRG und/oder
• - die zweite Energieaufbereitungsvorrichtung SRG2 und/oder
• - die Energiereserve BENG und/oder
• - die zweite Energiereserve BENG2 und/oder
• - die Trennvorrichtung TS und/oder
• - die Ladevorrichtung LDV.

In some special versions of the deployable quantum computer QC, it makes sense for electronic device parts of the quantum computer QC to be at least partially designed in radiation-hard electronics. Such, preferably radiation-hard, device parts of the quantum computer QC can include, for example:

• - the control device µC and/or
• - the memory RAM, NVM of the control device µC and/or
• - the computer core CPU and/or
• - the data interface DBIF and/or
• - the internal data interface MDBIF and/or
• - the light source driver LDRV and/or
• - the waveform generator WFG and/or
• - the amplifier V and/or
• - the photodetector PD and/or
• - the first camera interface CIF and/or
• - the second camera interface ClF2 and/or
• - the first camera CM1 and/or
• - the second camera CM2 and/or
• - the temperature sensor ST and/or
• - the microwave and/or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms and/or
• - the magnetic field sensors MSx, MSy, MSz and/or
• - the magnetic field controls MFSx, MFSy, MFSz and/or
• - the first energy processing device SRG and/or
• - the second energy processing device SRG2 and/or
• - the energy reserve BENG and/or
• - the second energy reserve BENG2 and/or
• - the separating device TS and/or
• - the LDV loading device.

In the sense of the document presented here, radiation-hard means that these functional elements of the quantum computer QC are intended and/or suitable for use in space and/or in areas of increased ionizing radiation, such as nuclear reactors or the environment of thermonuclear batteries.

In many applications, it is advantageous if the deployable quantum computer QC has a control device μC, which at least temporarily executes a neural network model. The neural network model that the control device µC typically executes processes input values and/or the values of input signals. The neural network model that the control device µC typically executes outputs output signals and/or output values of output signals. The control device µC then preferably influences states of quantum dots NV1, NV2, NV3 and/or states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ as a function of output signals and/or output values of the neural network model that the control device µC typically executes , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . Conversely, the control device µC preferably influences input signals depending on states of quantum dots NV1, NV2, NV3 and/or states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or input values of the neural network model that the control device µC typically executes.

Thus, the document presented here discloses, among other things, a smartphone and/or a portable quantum computer system and/or a mobile quantum computer system and/or vehicle and/or robot and/or aircraft and/or missile and/or Satellite and/or a rum missile and/or space station and/or floating body and/or ship and/or underwater vehicle and/or surface floating body and/or underwater floating body and/or deployable weapon system and/or warhead and/or surface or underwater vehicle and/or projectile and/or other mobile device and/or movable device. For the sake of simplicity, the document presented here refers to all of these as “vehicles”. The document presented here therefore proposes a vehicle in this very broad sense, which includes a deployable quantum computer QC, as described above. Conversely, the document presented here proposes a deployable quantum computer as previously described, which is a vehicle in the broad sense described above.

In a further, preferred variant, the quantum computer QC is intended to decrypt and/or encrypt the data communication, in particular of the control device μC, via a data interface DBIF. This is preferably the data interface DBIF of the control device µC. For this purpose, the control device µC preferably executes a cryptographic program 25, which encrypts or decrypts data that the control device µC receives via the data interface DBIF. Preferably, the control device μC uses the cryptography program 25 to carry out a method that is a post-quantum secure cryptography method for data from the quantum computer QC. This data from the quantum computer QC can be data that the quantum computer QC, or the control device µC, receives or sends out via the data interface DBIF, and can be other data.

A PQC-capable cryptography program 25 can, for example, be a “lattice-based” cryptography or so-called hash-based cryptography method based on multivariant equations, such as the “Rainbow” scheme. For example, it can be older NTRU procedures or GGH procedures or newer NTRU signature and BLISS signature procedures. The disadvantage of hash-based cryptography methods is the limited number of signatures that are possible. Furthermore, it can involve multivariant cryptography methods. These may include error-correcting cryptographic systems including McElience and Niedermeyer encryption algorithms. The Courtosis Finiasz and Sendier signature techniques are assigned to these as possible signature methods. or code-based cryptography. Other possible cryptography methods are cryptography methods for the cryptography program 25, which belong to the group of super singular elliptic curve isogeny cryptography. Such cryptographic systems, which come into question as cryptography program 25, use the mathematics of supersingular elliptic curves to enable a Diffie-Hellman key exchange between the control device μC of the quantum computer QC and another computer system via the data interface DBIF. In this context, the document presented here refers, as an example, to the Wikipedia statements under the link https://en.wikipedia.org/wiki/Supersingular_isogeny_key_exchange. The relevant document is attached as an appendix to this document and forms a full part of the disclosure presented herein.

Furthermore, the document presented here refers to the Wikipedia article https://en.wikipedia.org/wiki/Post-quantum_cryptography, which is also attached to this document and is part of the disclosure of the technical teachings of this document.

The said article mentions the methods Lattice-based cryptography, Multivariate cryptography, Hash-based cryptography, Code-based cryptography, Supersingular elliptic curve isogeny cryptography, Quantum resistance symmetric key (In English: Lattice-based cryptography, Multivariate cryptography, Hash-based cryptography, Code-based cryptography, Supersingular elliptic curve isogeny cryptography, Symmetric key quantum resistance) These and other post-quantum cryptography methods come as cryptography methods, cryptography methods for the cryptography program 25 in question, which executes the control device µC of the quantum computer QC and quantum computer-safe with other conventional computer systems and /or quantum computers to communicate.

Such a vehicle preferably includes sensors and/or measuring means in the broadest sense, which transmit measured values about the surroundings of the vehicle and/or conditions of the vehicle and/or conditions of the vehicle occupants or users of the vehicle and/or conditions of the vehicle's payload to the Supply control device µC. Under certain circumstances, the control device µC also receives measured values about the vehicle's surroundings via the DBIF data interface.

The control device μC preferably executes one or more measured value acquisition programs 26 to query the measured values and to control and monitor the associated measuring systems. The control device μC of the quantum computer QC can preferably use a vehicle condition determination program 26 to make a position assessment for the overall condition of the vehicle and/or the environment depending on such measured values of the vehicle. The overall condition of the vehicle in the sense of the document presented here can include the condition of the vehicle's surroundings and/or the condition of the vehicle occupants and/or the condition of the vehicle's load.

• - ein Radar-Sensor und/oder
• - ein Mikrofon und/oder
• - ein Ultraschalmikrofon und/oder
• - ein Infraschallmikrofon und/oder
• - einen Ultraschalltransducer und/oder
• - einen Infrarotsensor und/oder
• - einen Gassensor und/oder
• - einen Beschleunigungssensor und/oder
• - ein Geschwindigkeitssensor und/oder
• - einen Strahlungsdetektor und/oder
• - ein bildgebendes System und/oder
• - eine Kamera und/oder
• - eine Infrarotkamera und/oder
• - eine Multispektralkamera und/oder
• - ein LIDAR-System und/oder
• - ein Ultraschallmesssystem und/oder
• - ein Dopplerradarsystem und/oder
• - ein Quantenradarsystem und/oder
• - ein Quantensensor und/oder
• - ein Positionssensor und/oder
• - ein Navigationssystem und/oder
• - ein GPS-Sensor (oder eine funktionsäquivalente Vorrichtung) und/oder
• - ein Lagesensor und/oder
• - ein Partikelzähler und/oder
• - ein Detektionssystem für biologische Stoffe, insbesondere für biologische Kampstoffe,

und/oder

• - ein Gravimeter und/oder
• - ein Kompass und/oder
• - ein Gyroskop und/oder
• - ein MEMS-Sensor und/oder
• - ein Drucksensor und/oder
• - ein Neigungswinkelsensor und/oder
• - ein Temperatursensor und/oder
• - ein Feuchtesensor und/oder
• - ein Windgeschwindigkeitssensor und/oder
• - ein Wellenfrontsensor und/oder
• - ein mikrofluidisches Messsystem und/oder
• - ein Abstandsmesssystem und/oder
• - ein Längenmesssystem und/oder
• - ein biologischer Sensor zur Detektion biologischer Marker und/oder Viren und/oder Mikroben oder dergleichen und/oder
• - ein Sensorsystem zur Erfassung biologischer Messwerte von Fahrzeuginsassen und/oder zur Erfassung biologischer Messwerte lebender Ladung, insbesondere von Tieren und/oder biologischen Materialien,
• - ein Sitz-Belegungs-Messystem und/oder
• - ein Spannungssensor und/oder ein Stromsensor und/oder ein Leistungssensor.

In a further form, the document presented here proposes that at least one or more sensors SENS of the vehicle is one of the following sensors SENS providing measured values or comprises at least one of the following sensors SENS providing measured values as a subsystem:

• - a radar sensor and/or
• - a microphone and/or
• - an ultrasound microphone and/or
• - an infrasonic microphone and/or
• - an ultrasound transducer and/or
• - an infrared sensor and/or
• - a gas sensor and/or
• - an acceleration sensor and/or
• - a speed sensor and/or
• - a radiation detector and/or
• - an imaging system and/or
• - a camera and/or
• - an infrared camera and/or
• - a multispectral camera and/or
• - a LIDAR system and/or
• - an ultrasound measuring system and/or
• - a Doppler radar system and/or
• - a quantum radar system and/or
• - a quantum sensor and/or
• - a position sensor and/or
• - a navigation system and/or
• - a GPS sensor (or a functionally equivalent device) and/or
• - a position sensor and/or
• - a particle counter and/or
• - a detection system for biological substances, in particular for biological chemicals,

and or

• - a gravimeter and/or
• - a compass and/or
• - a gyroscope and/or
• - a MEMS sensor and/or
• - a pressure sensor and/or
• - an inclination angle sensor and/or
• - a temperature sensor and/or
• - a humidity sensor and/or
• - a wind speed sensor and/or
• - a wavefront sensor and/or
• - a microfluidic measuring system and/or
• - a distance measuring system and/or
• - a length measuring system and/or
• - a biological sensor for detecting biological markers and/or viruses and/or microbes or the like and/or
• - a sensor system for recording biological measurements of vehicle occupants and/or for recording biological measurements of living cargo, in particular of animals and/or biological materials,
• - a seat occupancy measurement system and/or
• - a voltage sensor and/or a current sensor and/or a power sensor.

As a consistent further development, the document presented here proposes a vehicle in the broad sense described above, in which the control device μC of the quantum computer QC controls the vehicle and/or device parts of the vehicle and/or a control of the vehicle or a device part depending on these measured values of the vehicle is influenced by a vehicle control program as an example of an application program 2. The control device μC of the quantum computer QC in preferably executes the vehicle control program as an example of an application program 2. The quantum computer QC preferably evaluates the sensor data of the sensors SENS and preferably changes at least temporarily the states of one or more quantum dots (NV1, NV2) of one or more quantum computers of the quantum computers QC1, QC2 depending on the values of the sensor data of the sensors SENS in direct or indirectly, especially after processing by the computer core CPU or another data processing system.

The document presented here further proposes a variant in which the vehicle has an interior and in which the control device μC of the quantum computer QC controls parameters of the interior of the vehicle and/or a device part in the interior of the vehicle by means of an interior con trollprograms as an example of an application program 2 influenced. The control device µC of the quantum computer QC in preferably executes the interior control program as an example of an application program 2.

The technical teaching presented here reveals in particular that the vehicle can be a weapon system and/or that the vehicle can include a weapon system that is coupled to the quantum computer QC.

For military applications, the vehicle may include a fire control system. The fire control system can in turn comprise one or more quantum computers QC and/or be coupled to one or more quantum computers QC, in particular the control device μC of the quantum computer QC. The control of the weapon system by the fire control system preferably depends at least temporarily on the quantum computer QC and its signaling, or the signaling of the control device μC of the quantum computer QC. The weapon system is controlled by the fire control system preferably in interaction between the fire control system and the QC quantum computer.

The vehicle preferably comprises an evaluation device which classifies the intended control of the weapon system with regard to the expected effects before the control is carried out and determines a control command class. The evaluation device preferably prevents execution of the control or postpones this execution until it is released by a human user if the control command determined in cooperation with the quantum computer QC falls into a predetermined control class. The evaluation device can be the control device μC of the quantum computer QC, which executes an evaluation program as an application program 2.

The vehicle can, for example, identify one or more targets with the aid of the evaluation program of the deployable quantum computer QC and/or with the aid of the deployable quantum computer QC. The neural network program is preferably an application program 2. The neural network program preferably includes classical algorithms 4, which classical hardware 6 executes using classical software 5. The control device µC of the quantum computer QC is preferably classical hardware 6. The neural network program that preferably executes the control device µC therefore preferably includes a classical algorithm 4, which the control device µC executes as classic hardware 6 using classical software 5.

The vehicle can then, for example, classify the one or more targets with the aid of the deployable quantum computer QC, in particular with the aid of a target classification program in the form of a neural network program. The target classification program is again preferably an exemplary possible application program 2, which, for example, a control computer µC of the deployable quantum computer QC can execute as classical hardware 6.

The application programs 2, which the quantum computer QC executes, preferably use classical hardware 6, which executes classical algorithms 4 using classical software 5, and quantum algorithms 7, which the quantum processor of the quantum computer QC executes. (please refer 5 ). The quantum algorithms 7 preferably have a predetermined temporal sequence of quantum gates, such as an X-gate, a CCNOT, a CNOT, a Hadamard gate, etc. Binary quantum op codes in the memory RAM, NVM of the control device µC preferably encode these quantum gates of the quantum algorithms 7. These binary quantum op codes also encode these quantum algorithms 7 as a compilation and sequence of quantum gates in the form of compilations and sequences of binary quantum algorithms. Op codes that symbolize these quantum gates. These binary quantum op codes are preferably stored together with classic binary command codes as quantum algorithms 7 in the memory RAM, NVM of the control device µC.

A list of quantum gates can be found on the Internet at Wikipedia, for example, under the link https://de.wikipedia.org/wiki/Liste_der_Quantengatter. This list is part of the disclosure description of the document presented here and is submitted with the registration of this document.

1. 1. das Identitäts-Gatter, das eine Identität des hyperkomplexen Eingangs erzeugt und daher keine Veränderung am Quantenzustand hervorruft,
2. 2. das Pauli-X-Gatter oder Nicht-Gatter, das eine Spiegelung des hyperkomplexen Eingangs an der X-Achse vornimmt,
3. 3. das Pauli-Y-Gatter, das eine Spiegelung des hyperkomplexen Eingangs an der Y-Achse vornimmt,
4. 4. das Pauli-Z-Gatter, das eine Spiegelung des hyperkomplexen Eingangs an der Z-Achse vornimmt,
5. 5. das Hadamard-Gatter, das eine Spiegelung des hyperkomplexen Eingangs an der X+Z-Achse vornimmt,
6. 6. das X-Rotationsgatter (auch als $\sqrt{NOT}\text{-Gatter}$
   
   bezeichnet), das den komplexen Eingang 90° (π/2) um die X-Achse dreht,
7. 7. das Y-Rotationsgatter, das den hyperkomplexen Eingang 90° (π/2) um die Y-Achse dreht,
8. 8. das (-X)-Rotationsgatter, das den komplexen Eingang -90° (-π/2) um die X-Achse dreht,
9. 9. das (-Y)-Rotationsgatter, das den hyperkomplexen Eingang -90° (-π/2) um die Y-Achse dreht,
10. 10. das S-Gatter oder Phasengatter(auch als $\sqrt{Z}\text{-Gatter}$
    
    bezeichnet), das die Phase 90° (π/2) um die Z-Achse dreht,
11. 11. das T-Gatter oder π/8-Gatter Phasen(schieber)gatter (auch als $\sqrt{S}\text{-Gatter}$
    
    bezeichnet), das die Phase 45° (π/4) um die Z-Achse dreht,
12. 12. das allgemeine Phasen(schieber)gatter, bei dem typischerweise k willkürlich festgelegt wird und das die Phase π/2k um die Z-Achse dreht,
13. 13. das willkürliche, unitäre Gatter, bei dem alle Eigenschaften werden willkürlich festgelegt werden

For example, single-input quantum gates include:

1. 1. the identity gate, which creates an identity of the hypercomplex input and therefore does not cause any change to the quantum state,
2. 2. the Pauli X gate or non-gate, which performs a reflection of the hypercomplex input on the X axis,
3. 3. the Pauli Y gate, which mirrors the hypercomplex input on the Y axis,
4. 4. the Pauli Z gate, which mirrors the hypercomplex input on the Z axis,
5. 5. the Hadamard gate, which mirrors the hypercomplex input on the X+Z axis,
6. 6. the X rotation gate (also called $\sqrt{NOT}\text{-Gate}$
   
   denotes), which rotates the complex input 90° (π/2) around the X axis,
7. 7. the Y rotation gate, which rotates the hypercomplex input 90° (π/2) around the Y axis,
8. 8. the (-X) rotation gate, which rotates the complex input -90° (-π/2) around the X axis,
9. 9. the (-Y) rotation gate, which rotates the hypercomplex input -90° (-π/2) around the Y axis,
10. 10. the S-gate or phase gate (also called $\sqrt{Z}\text{-Gate}$
    
    denotes), which rotates the phase 90° (π/2) around the Z axis,
11. 11. the T gate or π/8 gate phase (shifter) gate (also called $\sqrt{S}\text{-Gate}$
    
    referred to), which rotates the phase 45° (π/4) around the Z axis,
12. 12. the general phase (shifter) gate, where k is typically set arbitrarily and which rotates the phase π/2k about the Z axis,
13. 13. the arbitrary, unitary gate, in which all properties are arbitrarily determined

In the sense of the document presented here, the Z axis represents the real value, the X and Y axes (the phase position.

1. 1. das kontrollierte-Nicht-Gatter (CNOT, XOR-Verknüpfung), das den reellen Wert des zweiten Qubits (B) in Abhängigkeit vom reellen Wert des ersten Qubits (A) entweder beibehält (A=0) oder negiert (A=1) und den Wert des ersten Qubits beibehält.
2. 2. das Austausch-Gatter oder der Austauschknoten („Swap“), das die beiden Eingangs-Qubits vertauscht,
3. 3. das Wurzel Swap-Gatter, das als universelles Gatter die Eingangs-Qubits halb vertauscht,
4. 4. das Kontrollierte Z-flip Gatter (CZ) (Auch als kontrolliertes Z-Gatter, kontrollierter Phasenflip (CPF) oder Controlled-SIGN (CSIGN) bezeichnet)
5. 5. das kontrollierte Phasen-Gatter (C-Phase)
6. 6. das kontrollierte U-Gatter, das das zweite Qubit gemäß einer unitären Abbildung U transformiert, falls das erste Qubit den Wert „1“ hat und bleibt ansonsten unverändert. (C-NOT und C-Phase sind Spezialfälle von C-U),
7. 7. das Beliebige unitäre Transformations-Gatter, bei die unabhängigen Variablen der komplexen unitären 4x4-Matrix (16 reelle Parameter) können beliebig gewählt werden können, sodass das Gatter auf diese Weise alle Wechselwirkungen zwischen den beiden Qubits je nach Parameterwahl ausführen kann.

For example, quantum gates that refer to two quantum bits A, B include:

1. 1. the controlled-not gate (CNOT, XOR connection), which either maintains (A=0) or negates (A=1) the real value of the second qubit (B) depending on the real value of the first qubit (A). ) and retains the value of the first qubit.
2. 2. the exchange gate or node (“swap”), which swaps the two input qubits,
3. 3. the root swap gate, which, as a universal gate, half-swap the input qubits,
4. 4. the Controlled Z-flip Gate (CZ) (Also called Controlled Z-Gate, Controlled Phase Flip (CPF) or Controlled-SIGN (CSIGN))
5. 5. the controlled phase gate (C-phase)
6. 6. the controlled U gate, which transforms the second qubit according to a unitary mapping U if the first qubit has the value “1” and otherwise remains unchanged. (C-NOT and C-Phase are special cases of CU),
7. 7. the arbitrary unitary transformation gate, in which the independent variables of the complex unitary 4x4 matrix (16 real parameters) can be chosen arbitrarily, so that the gate can carry out all interactions between the two qubits depending on the choice of parameters.

1. 1. das Toffoli-Gatter bei dem das Gatter die ersten beiden Qubits (A und B) unverändert lässt und den reellen Wert des dritten Qubits (C) negiert, wenn der reelle Wert der ersten beiden Qubits positiv (d. h. logisch 1) ist, wodurch das Toffoli-Gatter logische AND-, XOR-, NOT- und FANOUT-Operationen durchführen kann und wodurch es universell für klassische Berechnungen eingesetzt werden kann.
2. 2. das Fredkin-Gatter, das das zweite und dritte Qubit vertauscht, wenn der reelle Wert des ersten Qubits negativ (d. h. logisch 0) ist.
3. 3. das Deutsch-Gatter, das ein universelles Drei-Qubit-Gatter ist, das beliebige Wechselwirkungen der ersten beiden Qubits auf das dritte Qubit durchführen kann und das die ersten beiden Qubits nicht verändert.

Quantum gates that refer to three quantum bits include, for example:

1. 1. the Toffoli gate in which the gate leaves the first two qubits (A and B) unchanged and negates the real value of the third qubit (C) if the real value of the first two qubits is positive (i.e. logical 1), whereby the Toffoli gate can perform logical AND, XOR, NOT and FANOUT operations, making it universally applicable for classical calculations.
2. 2. the Fredkin gate, which swaps the second and third qubits when the real value of the first qubit is negative (i.e. logical 0).
3. 3. the Deutsch gate, which is a universal three-qubit gate that can perform arbitrary interactions of the first two qubits on the third qubit and that does not change the first two qubits.

For further details, the document presented here refers to the font https://de.wikipedia.org/wiki/Liste_der_Quantengatter, which is to be viewed as an appendix to the description and part of the description and is attached to this application.

The quantum technological algorithms 7 now include individual quantum gates and/or compilations of quantum gates and/or sequences of such quantum gates and/or names of sequences of such quantum gates and/or sequences of names of sequences of such quantum gates and/or names of sequences of names of sequences of such quantum gates .

For this purpose, the quantum technology algorithms 7 typically include binary coded symbols of abstract quantum gate models 8 as quantum op codes for these quantum gates.

The contents of the memory RAM, NVM of the control device µC and/or a register of the control device µC preferably comprise a quantum program address counter.

The control device µC preferably identifies the current quantum op code using the value of the quantum program address counter current, binary coded symbol of the quantum gate model of the quantum gate models 8 that is currently to be executed. The control device μC then preferably identifies the quantum gate to be executed based on this current binary coded symbol of the abstract quantum gate models 8.

Possible influence 1: optical influence

According to the quantum gate to be executed, the control device µC controls the quantum points NV1, NV2, NV3 of the quantum computer QC in the predetermined quantum gate-specific manner according to a quantum gate hardware model 11 of the quantum gate currently to be executed. For this purpose, the control device µC controls and controls the waveform generator WFG and the light source driver LDRV and thus the light source LD by means of an SPc laser control program 13 for controlling and controlling the waveform generator WFG and the light source driver LDRV. Through this control and control of the waveform generator WFG and the light source driver LDRV and thus the light source LD, the control device μC can thus act on the quantum dots NV1, NV2, NV3 of the quantum computer QC in a quantum gate-specific manner by means of the pump radiation LB of the light source LD.

Possible impact 2: Impact via HF and microwave fields

According to the quantum gate to be executed, the control device µC controls the quantum points NV1, NV2, NV3 of the quantum computer QC and, if necessary, now also the core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC in the predetermined quantum gate-specific manner according to a quantum gate hardware model 11 of the quantum gate currently to be executed. For this purpose, the control device µC controls and controls the one or more microwave and/or radio wave frequency generators MW/RF-AWFG to generate an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3, to act on the quantum dots NV1, NV2, NV3 of the Quantum computer QC and/or the quantum states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC.

Here, the one or more microwave and/or radio wave frequency generators MW/RF-AWFG feed a transmission signal into one or more microwave and/or radio wave antennas mWA. Particularly preferably, the one or more microwave and/or radio wave antennas mWA comprise vertical lines LV1, LV2 or horizontal lines LH1, which are preferably located directly on the surface of the substrate D in the immediate vicinity (less than 30 nm) of the quantum dots NV1, NV2, NV3. This signal injection typically leads to electrical currents IH1, IV1, IV2 in these lines LH1, LV1, LV2, which in turn cause magnetic fields that are based on the magnetic dipole moments of the quantum dots NV1, NV2, NV3 of the quantum computer QC and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC. For this purpose, the control device preferably executes a control program 12 of the quantum gate hardware model 11 for the control and control of the one or more microwave and/or radio wave frequency generators MW/RF-AWFG. As a result, after the one or more microwave and/or radio wave frequency generators MW/RF-AWFG have been parameterized in a quantum gate-specific manner, the one or more microwave and/or radio wave frequency generators MW/RF-AWFG generate an electromagnetic wave field in a quantum gate-specific manner by means of one or more microwaves - and/or radio wave antenna mWA, in particular the said vertical lines LV1, LV2 or horizontal lines LH1, at the respective location of the quantum dots NV1, NV2, NV3, to act on the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the Core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC. This enables the targeted manipulation of the quantum states of the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC in a quantum gate-specific manner.

Typically, the control device µC carries out the manipulations of the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC by means of the light source LD and one or more microwave and/or radio wave antennas mWA, if applicable, synchronized in time in a quantum gate-specific manner and, if necessary, also in parallel in time.

To generate a quantum gate, the control device µC controls the light source driver LDRV and thus the light source LD by means of a quantum gate-specific sequence of signals from the waveform generator WFG by means of a transmission signal S5. The resulting quantum gate-specific sequence of signals from the light source LD then manipulates the quantum dots NV1, NV2, NV3 of the quantum computer QC in the predetermined quantum gate-specific manner. The quantum gate hardware model 11 includes the SPc Laser-Kon Trolling program 13 for the control and control of the waveform generator WFG and the light source driver LDRV and thus the light source LD, which acts on the quantum dots NV1, NV2, NV3 of the quantum computer QC by means of the pump radiation LB of the light source LD. The control device µC uses this SPc laser control program 13 using suitable parameters, such as laser intensity and laser pulse length, by which the quantum dots NV1, NV2, NV3 of the quantum computer QC correspond in the predetermined quantum gate-specific manner to the currently processed binary quantum op code of the quantum technology algorithm 7. According to the value of the quantum program counter. After the execution of the currently processed binary quantum op code of the quantum technological algorithm 7. The quantum computer and / or the control device µC increases the quantum program counter of the quantum computer by the instruction length of the quantum op code. The quantum op-code instruction length typically includes the lengths of the quantum op-code itself plus the sum of the lengths of the quantum op-code's parameters. The parameters of the quantum OP code can, for example, be the quantum dots NV1, NV2, NV3 to be controlled and/or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ describe.

After parameterization by the control device µC, the waveform generator WFG controls the light source driver LDRV and thus the light source LD in a quantum gate-specific manner with a transmission signal S5 with a quantum gate-specific transmission signal curve. Controlled by the control device µC, the waveform generator WFG generates the transmission signal S5 to generate a quantum gate, preferably in a time-synchronized manner to the radio frequency and microwave signals from the microwave and/or radio wave frequency generator MW/RF-AWFG.

To generate a quantum gate of an abstract quantum gate model 8, a quantum gate-specific sequence of signals from the one or more microwave and / or radio wave frequency generators MW / RF-AWFG typically radiates in parallel in time by means of one or more microwave and / or radio wave antennas mWA Substrate D. The one or more microwave and/or radio wave antennas mWA thus irradiate the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in a fixed temporal phase relationship to the light pulses of the light source LD during the irradiation of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ with pump radiation LB through the light source LD in a quantum gate-specific manner. The one or more microwave and/or radio wave frequency generators MW/RF-AWFG are preferably suitable for generating waveforms that can be largely freely specified by the control device µC (English: arbitrary wave form generator).

The information in the memory RMA, NVM of the control device μC of the quantum computer QC preferably includes these quantum algorithms 7. The quantum algorithms 7 are preferably composed of sequences of said binary codes as symbols of the quantum gates of the abstract quantum gate models 8. Such a binary code preferably encodes a) the quantum gate of the abstract quantum gate models 8 and b) which quantum points NV1, NV2, NV3 of the quantum computer QC and/or core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC should use the control device µC as a participant in the quantum gate to be executed.

The control device μC preferably uses a transcompiler 9 to translate these binary codes of the quantum algorithms 7 into hardware commands of a quantum gate hardware model 11 for the various device parts for manipulating the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or for manipulating the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC and/or for reading out the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or for reading out the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC. The control device μC preferably uses the transcompiler 9 to optimize the used hardware instructions of the quantum gate hardware model 11 and their temporal sequence and, if necessary, adds additional hardware instructions of the quantum gate hardware model 11, for example for error correction. For the translation of the quantum algorithms 7 into hardware instructions of the quantum gate hardware model 11, the control device µC preferably uses hardware quantum gate description models in the form of the abstract quantum gate models 8 of a hardware quantum gate description model database 8, which is available to the transcompiler 9 as a library Quantum gate and instructions for its implementation using the existing hardware of the quantum computer QC according to the quantum gate hardware model 11. An entry for an abstract quantum gate model 8 of the hardware quantum gate description model database 8 includes a list of the temporal sequence ele for each available quantum gate of the quantum computer QC, preferably for each abstract quantum gate model 8 mental hardware operations (12, 13, 14, 17) of individual device parts of the quantum computer QC, which, depending on the circumstances, the quantum computer QC can also carry out completely or partially in parallel in time. Such an elementary hardware operation can, for example, involve the emission of a laser pulse of a defined length and intensity at a specific time or the generation of an HF or microwave signal with a predetermined microwave or HF frequency, duration and microwave or RF intensity with predefined phase position and time position to a time base and the like. The hardware operations can typically be divided into groups.

A first group of hardware operations of the quantum gate hardware model 11 includes the temporal sequence of the RF pulses and microwave pulses. This time sequence controls the control device μC by means of the said control program 12 for the control and control of the one or more microwave and / or radio wave frequency generators MW / RF-AWFG for generating an electromagnetic wave field by means of one or more microwave and / or radio wave antenna mWA, in particular vertical lines LV1, LV2 or horizontal lines LH1 at the respective location of the quantum dots NV1, NV2, NV3, for influencing the quantum states of the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC.

A second group of hardware operations of the quantum gate hardware model 11 includes a control program 13 for generating light pulses using the waveform generator WFG and the light source driver LDRV and the light source LD. This time sequence controls the control device µC by means of the said SPc laser control program 13 for the control and control of the waveform generator WFG and the light source driver LDRV and thus the light source LD, which is applied to the quantum states of the quantum dots NV1, NV2 by means of the pump radiation LB of the light source LD. NV3 of the quantum computer QC acts.

A third group of hardware operations of the quantum gate hardware model 11 includes a control program 14 for controlling, controlling and reading out values of the means PD, V for optically reading out the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the Quantum states of the core quantum dots CI1 ₁ , _{CI1 2} , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC by the control device µC.

A fourth group of hardware operations of the quantum gate hardware model 11 includes a control program 15 for execution by the control device µC for the control and / or control and / or regulation of a magnetic field generating device (MGx, MGy, MGy, MFSx, MFSy, MFSz) to generate an additional magnetic flux density at the location of the quantum dots (NV1, NV2, NV3) and/or at the location of the core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) of the quantum computer (QC). This control and/or control and/or regulation of the magnetic field generating device (MGx, MGy, MGy, MFSx, MFSy, MFSz) of the quantum computer (QC) is preferably carried out in parallel or quasi-parallel with the execution of the hardware commands in the form of the control programs (12 to 17, 22, 23). This control and/or control and/or regulation of the magnetic field generating device (MGx, MGy, MGy, MFSx, MFSy, MFSz) of the quantum computer (QC) is preferably carried out depending on the measured values recorded by the magnetic field measuring device (MSx, MSy, MSy, MFSx, MFSy, MFSz) for recording the magnetic flux density at the location of the quantum dots (NV1, NV2, NV3) and/or at the location of the core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1, CI2 ₂ , _{CI2 3 ,} CI3 ₁ , CI3 ₂ , CI3 ₃ ) of the quantum computer (QC).

A fifth group of hardware operations of the quantum gate hardware model 11 includes a control program 16 for execution by the control device µC and for controlling and controlling the optical system OS in order to optimize the irradiation of the laser beam LB into the substrate D if necessary . With the help of the control program 16 for controlling the optical system OS, the control device μC can, for example, preferably adjust the focus of the optical system OS or other parameters of the optical system so that the function of the quantum computer QC is approximately optimal.

A sixth group of hardware operations of the quantum gate hardware model 11 includes a control program 17 for execution by the control device µC and for controlling and adjusting DC current levels and/or DC voltage levels to influence specific quantum dots NV1, NV2, NV3 of the quantum computer QC and/or certain core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC in such a way that they may not be connected to a hardware participate in an operation or take part in a hardware operation. In this context, the document presented here refers to the technical teaching of DE 10 2020 125 189 A1 . The scalability of the QC quantum computer presented here is further explained there.

A seventh group of hardware operations of the quantum gate hardware model 11 includes a control program 22 for execution by the control device µC and for controlling and adjusting the position and/or alignment of the substrate D with the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 _{1 , CI2 2 ,} CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC compared to the optical system OS. The control device µC can use this control program 22 for execution by the control device µC and for controlling and adjusting the position and/or alignment of the substrate D with the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 3 , CI3 ₁ , CI3 ₂ , CI3 _{3 of} the quantum computer QC relative to the optical system OS and, for example, by means of a translational positioning device in the X direction XT and / or a translational positioning device in the Y direction YT and possibly further alignment devices, the position and/or the alignment of the substrate D with the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , Change CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC compared to the optical system OS. This control program preferably evaluates 22 measured values of device parts (CIF, CM1, CIF2, CM'', LM) to record the position and/or the alignment of the substrate D with the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1, CI2 ₂ , _{CI2 3} , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC compared to the optical system OS and optimized depending on the measured values recorded in this way for the position and/or the Alignment of the substrate D with the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC opposite the optical system OS by means of the alignment and positioning devices, the position and/or the alignment of the substrate D with the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC compared to the optical system OS.

An eighth group of hardware operations of the quantum gate hardware model 11 includes a control program 23 for execution by the control device µC and for controlling and adjusting the temperature of the material of the substrate D with the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or or the core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , Cl2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC. For this purpose, the control device μC preferably detects at least one temperature measurement value of this temperature or a temperature close to it using this control program 23 and a temperature sensor ST and regulates this temperature measurement value to a temperature target value using this program 23 and cooling devices KV, HeCLCS.

With the help of the hardware operations of the quantum gate hardware model 11, the control device µC can access the specific quantum points NV1, NV2, NV3 of the quantum computer QC and/or specific core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC access and manipulate and/or read them.

To address individual specific quantum points NV1, NV2, NV3 of the quantum computer QC and/or individual specific core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC include Hardware operations of the quantum gate hardware model 11 prefers the necessary quantum dot or core quantum dot specific access data sets. An access data set preferably includes information about the method with which the relevant quantum dot or the relevant core quantum dot can be manipulated and which parameters are necessary for this. For example, the access data set can include the frequencies for controlling the quantum dot or core quantum dot. In this context, the document presented here refers to the technical teaching of DE 10 2020 125 189 A1 .

In the case of a vehicle for military purposes or a weapon system, the vehicle or weapon system can use the quantum computer QC and a prioritization program to determine a chronological order or prioritization of combating multiple targets. The prioritization program is preferably an application program 2, which preferably executes the control device μC.

In the case of a vehicle for military purposes or a weapon system, the vehicle or the weapon system can use the quantum computer QC to determine a time to combat a target using a time determination program. The time determination program is preferably an application program 2, which preferably executes the control device μC.

In the case of a vehicle for military purposes or a weapon system, the vehicle or the weapon system can use the quantum computer QC to select a weapon type and/or an ammunition for combating a target by means of a selection determine program. The selection program is preferably an application program 2, which preferably executes the control device μC.

The document presented here suggests, among other things, a possible embodiment of a vehicle that uses the quantum computer QC to determine a route for the vehicle using a route determination program. The route determination program is preferably an application program 2, which preferably executes the control device μC.

In the case of a vehicle for military purposes or a weapon system, the vehicle or weapon system can use the quantum computer QC to determine a route for a weapon or a warhead or a projectile or an ammunition or another vehicle.

The document presented here also proposes, among other things, a vehicle in which the control device μC at least temporarily executes a neural network model as an application program 2 and in which the neural network model processes input values and/or input signals and outputs output signals and/or output values. As already described above, the control device µC typically influences states of the quantum dots NV1, NV2, NV3 and/or states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ depending on output signals and/or output values of the neural network model , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . In this embodiment, the control device typically influences μC depending on the states of the quantum dots NV1, NV2, NV3 and/or states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ input signals and/or input values of the neural network model.

Substrate

As described above, the deployable quantum computer QC according to the proposal comprises a substrate D with one or more quantum dots NV1, NV2, NV3. The substrate D preferably comprises diamond as the substrate material. The diamond is preferably isotopically pure or has at least one isotopically pure portion, which preferably has the quantum dots NV1, NV2, NV3. The quantum dots NV1, NV2, NV3 are preferably paramagnetic centers. In the case when the substrate material of the material of the substrate D comprises diamond, the paramagnetic centers are preferably ST1 centers and/or preferably TR1 centers and/or very particularly preferably NV centers. This means that interference caused by such isotopic impurities does not interfere with the functionality of the quantum bits, or at most only does so to a sufficiently small extent. In relation to diamond, this means that the diamond preferably consists essentially of ¹² C isotopes as base isotopes. Such ¹² C isotopes have no magnetic moment that can interact with the quantum dots NV1, NV2, NV3. The core quantum dots CI1 ₁ , CI1 ₂ , CI1 3 , CI2 1 , CI2 ₂ , _{CI2 3} , CI3 ₁ , _{CI3 2 ,} CI3 ₃ are preferably also located in the isotopically pure region of the substrate D. When we talk about isotope purity here, the isotopes that serve as core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are not taken into account when assessing the isotope purity . At this point, this writing specifically refers to Scripture DE 10 2020 125 189 A1 , whose technical teachings for the following international procedures, to the extent legally permissible in the relevant registration countries, are part of the disclosure of this document by reference. Isotopically pure within the meaning of this disclosure and the DE 10 2020 125 189 A1 is a material when the concentration of isotopes other than the base isotopes that dominate the material is so low that the technical purpose is achieved to a level sufficient for the production and sale of products with an economically sufficient production yield. The DE 10 2020 125 189 A1 lists the relevant isotope ratios of the relevant elements on which the technical teaching disclosed here is based. Since isotopically pure diamonds are extremely expensive, it makes sense if the substrate D comprises a diamond material and, for example, the diamond material comprises an epitaxially at least locally grown isotopically pure layer essentially made of ¹² C isotopes. This can be deposited, for example, using CVD and other deposition methods on the original surface of a silicon wafer used as substrate D or a diamond surface. From now on, the term substrate D includes the part of the combination of substrate D and epitaxially grown layer DEPI in which the quantum dots NV1, NV2, NV3 are manufactured. Typically this is the epitaxial layer DEPI. Essentially this means that the total proportion K _1G ' of the C isotopes with magnetic moment, which are part of the substrate D, based on 100% of the C atoms, which are part of the substrate D, compared to those in the tables of DE 10 2020 125 189 A1 specified natural total proportion K _1G is reduced to a proportion K _1G 'of the C isotopes with magnetic moment which are part of the substrate D, based on 100% of the C isotopes which are part of the substrate D. This proportion K _1G ' is preferably smaller than 50%, better smaller than 20%, better smaller than 10%, better smaller than 5%, better smaller than 2%, better smaller than 1%, better smaller than 0.5% , better less than 0.2%, better less than 0.1% of the natural total proportion K _1G for C isotopes with magnetic moment on the C isotopes of Substrate D in the area of influence of the quantum dots NV1, NV2, NV3 and/or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . When determining the proportion K _1G ', those C atoms of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are not taken into account, since their magnetic moments are intentional and are therefore not parasitic.

The use of NV centers and/or ST1 centers and/or TR12 centers or L1 centers as quantum dots NV1, NV2, NV3 of the quantum bits of the quantum computer QC enables the operation of the quantum computer QC at room temperature and thus the ability to deploy it in the first place Quantum Computer QC. The electron spin configuration of such a paramagnetic center serves as a quantum dot of the quantum dots NV1, NV2, NV3. In addition to such quantum dots NV1, NV2, NV3 as quantum bits, the deployable quantum computer QC preferably also includes nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ as nuclear core quantum bits. Typically, the magnetic moments of isotopes that have non-zero magnetic moments due to nuclear spin serve as nuclear nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . Such nuclear magnetic moments of the relevant isotopes of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ preferably couple with the electron configuration of the paramagnetic centers of the quantum dots NV1, NV2, NV3 . This allows a control device μC of the quantum computer QC to manipulate the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ by manipulating the states of the quantum dots NV1, NV2, NV3 . The control device μC can also read the nuclear quantum states of the nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ by electrically or optically reading out the quantum states of the quantum dots NV1, NV2 , Capture NV3. The control device µC can also couple core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ that are distant from one another by means of chains of coupled quantum dots NV1, NV2, NV3. The nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ thus form nuclear core quantum bits. In these nuclear quantum dots CI1 ₁ . CI1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ are preferably the nuclear spins of isotopes with a magnetic nuclear nuclear moment. These can also include the nuclei of nitrogen atoms (e.g. ¹⁵ N or ¹⁴ N) of NV centers and the nuclei of ¹³ C isotopes. At this point the document presented here expressly refers to the document again DE 10 2020 125 189 A1 , whose technical teachings for the following international procedures, to the extent legally permissible in the relevant registration countries, are part of the disclosure of this document by reference. The nuclear quantum dots Cl1 ₁ . Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the nuclear quantum bits are characterized by very long T2 times. The proposed deployable quantum computer QC preferably uses its quantum dots NV1, NV2, NV3 to control and entangle the states of the nuclear core quantum dots Cl1 ₁ . Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ . Cl3 ₂ , Cl3 ₃ and for reading out the nuclear quantum states of the nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 _{1 , Cl2 2 ,} Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . The quantum states of the quantum dots NV1, NV2, NV3 can be read out optically and/or electrically. With regard to electrical reading, this document expressly refers to the document
DE 10 2020 125 189 A1 , whose technical teachings for the following international procedures, to the extent legally permissible in the relevant registration countries, are part of the disclosure of the document presented here by reference. Another advantage of the deployable quantum computer QC proposed here is the relatively easy operation and the better selectivity of the control of the quantum dots NV1, NV2, NV3 and the quantum bits and the good scalability compared to other quantum computers.

As described above, a proposed quantum computer QC typically comprises a substrate D with one or more quantum dots NV1, NV2, NV3. In addition, the substrate D preferably also has one or more nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 1 , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , _{Cl3 2 ,} Cl3 ₃ . The quantum dots NV1, NV2, NV3 are preferably one or more paramagnetic centers which form one or more quantum bits. The nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ are preferably one or more isotopes with a magnetic moment, which form one or more nuclear quantum bits. The document presented here expressly refers again to this DE 10 2020 125 189 A1 . The nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ are therefore preferably the magnetic moments of isolated isotopes in the vicinity of the quantum dots NV1, NV2, NV3. Here, proximity means that there is a coupling of the magnetic moments of the isotopes in question, which form the nuclear quantum dots Cl1 ₁ . Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ form, with the nearby quantum dot of the nearby quantum bit is possible with the device presented here.

The quantum dots NV1, NV2, NV3 preferably have a magnetic moment of an electron configuration of the respective quantum dot. In the sense of the technical teaching of the document presented here, the quantum dots NV1, NV2, NV3 preferably couple to one another by means of this magnetic moment. One or more quantum dots NV1, NV2, NV3 are preferably paramagnetic centers in the substrate D. Preferably, the Fermi level of the substrate D in the area of a paramagnetic center used as a quantum dot is set so that the paramagnetic center is electrically charged. The electrical charge is preferably negative. In the case of an NV center as a paramagnetic center, the NV center is preferably negatively charged. In the case of an NV center as a paramagnetic center, the NV center is therefore preferably an NV ^- center. The NV centers in the substrate D therefore preferably include NV ^- centers. Doping the substrate D in the area of the paramagnetic center preferably ensures that the paramagnetic center is electrically charged in the intended manner. Isotopes without a magnetic moment as doping atoms preferably dope the material of the substrate D in the area of the relevant quantum dot of the quantum dots NV1, NV2, NV3. These doping atoms preferably shift the Fermi level in the area of this relevant quantum dot without a magnetic moment. These doping atoms therefore preferably shift the Fermi level in the area of the relevant paramagnetic center without a magnetic moment. Preferably, the substrate D essentially comprises, apart from the isotopes that serve as core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the core quantum bits, isotopes without a nuclear magnetic moment. Since the atoms of III. Main group of the periodic table and the V. Main group of the periodic table generally do not have any stable isotopes without a magnetic moment, so the material of the substrate (D) is preferably mixtures and / or compounds of isotopes without a magnetic moment, for example from isotopes of VI. Main group - e.g. ¹² C, ¹⁴ C, ²⁸ Si, ³⁰ Si, ⁷⁰ Ge, ⁷² Ge, ⁷⁴ Ge, ⁷⁶ Ge, ¹¹² Zn, ¹¹⁴ Zn, ¹¹⁶ Zn, ¹¹⁸ Zn, ¹²⁰ Zn, ¹²² Zn, ¹²⁴ Zn and/or the VI. Main group ¹⁶ E, ¹⁸ E, ³² S, ³⁴ S, ³⁶ S, ⁷⁴ Se, 76 Se, ⁷⁸ Se, ⁸⁰ Se, ⁸² Se, ¹²⁰ Te, ¹²² Te, ¹²⁴ Te, ¹²⁶ Te, ^{128 Te} , ¹³⁰ Te, and /or the II main group ²⁴ Mg ^{, 26} Mg, ⁴⁰ Ca, ⁴² Ca, 44 Ca, 46 Ca, ⁴⁸ Ca, ⁸⁴ Sr, ⁸⁶ Sr, ⁸⁸ Sr, ¹³⁰ Ba, ¹³² Ba ^{, 134} Ba, ¹³⁶ Ba, ¹³⁸ Ba , and/or the II subgroup ⁴⁶ Ti, ⁴⁸ Ti, ⁵⁰ Ti, ⁹⁰ Zr, ⁹⁰ Zr, ⁹² Zr, 94 Zr, ⁹⁶ Zr ^{, 174 Hf, 176 Hf, 178 Hf , and} /or the IV subgroup ⁵⁰ Cr , ⁵² Cr, ⁵³ Cr, ⁹² Mo, ⁹⁴ Mo, ⁹⁶ Mo, ⁹⁸ Mo, ¹⁰⁰ Mo, ¹⁸⁰ W, ¹⁸² W, ¹⁸⁴ W, ¹⁸⁶ W, and/or the VI. Subgroup ⁵⁴ Fe, ⁵⁶ Fe, ⁵⁸ Fe, ⁹⁶ Ru, ⁹⁸ Ru, ¹⁰⁰ Ru, ¹⁰² Ru, ¹⁰⁴ Ru, ¹⁸⁴ 0s, ¹⁸⁶ 0s, ¹⁸⁸ Os, ¹⁹⁰ Os, ¹⁹² Os and/or the VIII subgroup ⁵⁸ Ni, ⁶⁰ Ni, ⁶² Ni, ⁶⁴ Ni, ¹⁰² Pd, ¹⁰² Pd, 104 Pd ^{, 106} Pd, ¹⁰⁸ Pd, ¹¹⁰ Pd, ¹⁹⁰ Pt, ¹⁹² Pt, ¹⁹⁴ Pt, ¹⁹⁶ Pt, ¹⁹⁸ Pt and/or the X subgroup ⁶⁴ Zn, ⁶⁶ Zn, ⁶⁸ Zn, ⁷⁰ Zn, ^{106 Cd, 108} Cd, ¹¹⁰ Cd, ¹¹² Cd, ^{114 Cd} , ¹¹⁶ Cd, ¹⁹⁶ Hg, ¹⁹⁸ Hg, ²⁰⁰ Hg, ²⁰² Hg, ²⁰⁴ Hg and/or the lanthanides: ¹³⁶ Ce, ¹³⁸ Ce, ¹⁴⁰ Ce ^{, 142} Ce, 142 Nd, ¹⁴⁴ Nd, ¹⁴⁶ Nd, ¹⁴⁸ Nd, ¹⁵⁰ Nd, 144 Sm, ¹⁴⁶ Sm, ¹⁴⁸ Sm, ¹⁵⁰ Sm, ¹⁵² Sm, ¹⁵⁴ Sm, ¹⁵² Gd, ^{154 Gd} , ^1S6 Gd , ¹⁵⁸ Gd ^{, 160} Gd, ¹⁵⁶ Dy, ¹⁵⁸ Dy, 160 Dy, ¹⁶² Dy, ¹⁶⁴ Dy, ¹⁶² Er, ¹⁶⁴ Er, ¹⁶⁶ Er, ¹⁶⁸ Er, ¹⁷⁰ Er, ¹⁶⁸ Yb, ¹⁷⁰ Yb, ¹⁷² Yb, ¹⁷⁴ Yb, ¹⁷⁶ Yb, and/or the actinides ²³² Th, ²³⁴ Pa, ²³⁴ U, ²³⁸ U, ²⁴⁴ Pu in question. These isotopes can also be used as doping atoms for doping the substrate (D). If the substrate D comprises diamond and if the quantum dots NV1, NV2, NV3 comprise paramagnetic centers, ³² S, ³⁴ S, ³⁶ S, ¹⁶ O and ¹⁸ O are preferred as doping isotopes for shifting the Fermi level. For the formation of NV centers in diamond as substrate D, an advantageous effect can also be observed for doping with phosphorus, although this is less optimal. The phosphorus isotopes typically have a magnetic moment that interacts with the electron configuration of the paramagnetic centers. However, this interaction is typically undesirable.

Light source LD

According to the proposal, the proposed deployable quantum computer QC preferably comprises a light source LD. The light source LD is preferably a laser which can irradiate quantum dots NV1, NV2, NV3 of the deployable quantum computer with pump radiation LB of a pump radiation wavelength λ _pmp . The light source LD preferably irradiates the relevant quantum dots NV1, NV2, NV3 with pump radiation LB, which is pulse-modulated in its time intensity profile, i.e. preferably pulsed.

Preferably, the light source LD can emit light pulses of the pump radiation LB at light pulse start times t _sp that can be predetermined by the control device µC, based on a reference time t _0p , with a light pulse duration t _dp . A control device µC of the deployable quantum computer preferably controls the light source LD with the aid of a light source driver LDRV via a control data bus SDB. The light source driver LDRV supplies the light source LD with energy. This energy supply to the light source LED typically depends on control commands that the light source driver LDRV receives from the control device µC via the control data bus SDB. The radiation power of the pump radiation LB emitted by the light source LD typically depends on control commands that the light source driver LDRV receives from the control device μC via the control data bus SDB, and on one or more transmission signals S5. The light source is preferably LD around a semiconductor laser. Most preferably, the LED light source is a laser diode. The use of an LED (light-emitting diode) as a light source LD is also conceivable. In the exemplary use of NV centers as paramagnetic centers NV1, NV2, NV3 in diamond as quantum dots, the light from the light source LD used as pump radiation LB preferably has a wavelength in a wavelength range of 400 nm to 700 nm wavelength and/or better 450 nm to 650 nm and/or better 500 nm to 550 nm and/or better 515 nm to 540 nm. In the course of developing the technical content of this document, a wavelength of 532 nm of the electromagnetic radiation from the light source LD used as pump radiation LB gave good results. The light source LD preferably comprises a laser, which is preferably a semiconductor laser. In the case of NV centers as paramagnetic centers in diamond as substrate D, a laser diode from Osram of the type PLT5 520B with a 520 nm wavelength has proven itself as an exemplary light source LD for irradiating the NV centers in diamond with pump radiation LB. The deployable quantum computer QC according to the proposal preferably comprises said light source driver LDRV, which controls the emission of the pump radiation LB by the light source LD.

A waveform generator WFG preferably controls the light source driver LDRV and thus the light source LD by means of a transmission signal S5. The waveform generator WFG generates the transmission signal S5 preferably synchronized in time to the radio frequency and microwave signals that the microwave and / or radio wave frequency generator MW / RF-AWFG generates to generate largely freely definable waveforms (English: arbitrary wave form generator) and by means of a Microwave and / or radio wave antenna mWA radiates into the substrate D. The microwave and/or radio wave antenna mWA thus irradiates the quantum dots NV1, NV2, NV3 and the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ in a fixed time period Phase relationship to the light pulses of the irradiation of the irradiation of the quantum dots NV1, NV2, NV3 and the core quantum dots Cl1 ₁ . Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₁ , Cl3 ₃ with pump radiation LB through the light source LD. Typically, the microwave and/or radio wave frequency generator MW/RF-AWFG synchronizes itself to the waveform generator WFG on the transmission signal S5, preferably on the transmission signal S5. This ensures that the phase relationship between the radio and microwave signals from the microwave and/or radio wave frequency generator MW/RF-AWFG on the one hand and the light pulses from the light source LD on the other hand have a predeterminable phase relationship to one another. Preferably, the computer core CPU of the control device µC of the deployable quantum computer QC sets the operating parameters of the waveform generator WFG and the microwave and/or radio wave frequency generator MW/RF-AWFG in accordance with the desired quantum operation in such a way that the quantum states of the quantum dots NV1, NV2, NV3 and the Core quantum states of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ can be manipulated as intended.

The light source LD preferably comprises a photodetector. The system preferably includes light source LD and light source driver LDRV and a controller. The photodetector PD of the light source LD can be, for example, a photodiode, which typically monitors the intensity of the pump radiation LB emitted by the light source LD. The controller is preferably part of the light source driver LDRV. The light source driver LDRV preferably drives the light source LD depending on the transmission signal S5. The controller is preferably a P controller or better an I controller or better a PI controller or better a PID controller or a controller with a frequency-optimized frequency response of the gain of the open control loop or the loop gain. The controller preferably compares the value of the measurement signal from the photodetector of the light source LD with the transmission signal S5 from the waveform generator WFG. Depending on the comparison result of the value of the transmission signal S5 with the value of the measurement signal of the photodetector of the light source LD, the controller of the light source LD then regulates the intensity of the pump radiation LB. The controller of the light source LD preferably regulates the intensity of the pump radiation LB by changing the driving power of the light source driver LDRV. As a result, in the ideal case, in the steady state, the intensity of the pump radiation LB essentially corresponds to the value of the transmission signal S5, apart from control deviations. Ideally, the controller of the light source driver LDRV has an analog-to-digital converter and a data interface to the internal control data bus SDB of the deployable quantum computer QC. In this case, the controller and/or a control computer of the light source driver LDRV and/or a control computer of the light source LD can, for example, via the control data bus SDB of the deployable quantum computer QC, which are controlled by the controller of the light source driver LDRV of the light source LD and/or the control computer of the light source LD and / or provide the controller of the light source driver LDRV detected intensity values of the pump radiation LB to the control device µC of the deployable quantum computer QC. In this case, the controller and/or said control computer of the light source LD and/or the control computer of the light source LD can, for example, via the control data bus SDB of the deployable quantum computer QC the other operating parameters of the light source LD such as, for example, through an analog-to-digital converter and / or sensors within the light source LD and / or the light source driver LDRV, such as respective operating voltages, respective temperatures or the like of the control device µC of the deployable Quantum computer QC also provide. An amplifier of the light source LD and/or an amplifier of the light source driver LDRV preferably amplify the signal of the photodetector of the light source LD before, for example, the analog-to-digital converter of the controller of the light source driver LDRV converts this into a digital measurement signal for the controller of the light source driver LDRV Light source LD converts. The control device µC can, for example, configure the light source LD and/or the light source driver LDRV and their components via the control data bus SDB. Such configuration goals can, for example, but not only, the controller of the light source driver LDRV of the light source LD and its control parameters and / or the gain and / or the frequency response of the amplifier of the light source LD and / or the gain and / or the frequency response of the amplifier of the light source driver LDRV and be their parameters. The light source driver LDRV and the light source LD can form a unit. The light source driver LDRV and the light source LD can have one or more common control computers and/or one or more common analog-to-digital converters. For setting analog control parameters, the light source LD and/or the light source driver LD may have one or more digital-to-analog converters that provide analog control levels within the light source LD and/or the light source driver LD. The control device μC of the quantum computer QC preferably controls these digital-to-analog converters via the control data bus SDB. The possibly existing control computer of the light source LD and/or the possibly existing control computer of the LED driver LDRV can also control the digital-to-analog converters.

Optical system

The optical system OS preferably includes a confocal microscope. The light source LD emits the pump radiation LB. In the example of the 1 the pump radiation LB passes through the dichroic mirror DBS. The optical system OS focuses the pump radiation LB on quantum dots NV1, NV2, NV3 and/or nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ in the focal point of the optical System OS. The optical system OS prefers to use its confocal microscope. The irradiation of the quantum dots NV1, NV2, NV3 typically causes the quantum dots NV1, NV2, NV3 to emit fluorescent radiation FL. The optical system OS typically detects at least part of the fluorescence radiation FL of the quantum dots NV1, NV2, NV3. The optical system OS supplies this detected fluorescence radiation FL to the photodetector PD via the dichroic mirror DBS. The dichroic mirror DBS or another device preferably separates the pump radiation LB and the fluorescent radiation FL from one another in such a way that essentially only fluorescent radiation FL reaches the photodetector PD. Instead of a dichroic mirror DBS, the quantum computer QC proposed here can therefore also include a combination of a semi-transparent mirror and an optical filter. The optical filter is then preferably arranged relative to the semi-transparent mirror on the side of the photodetector PD. The optical filter then preferably allows radiation with the fluorescence wavelength λfl of the fluorescence radiation FL to pass through essentially undamped. The optical filter then preferably essentially does not allow radiation with the pump radiation wavelength λ _pmp of the pump radiation LB to pass through. In the example of the 1 the proposed quantum computer QC has another semi-transparent or partially reflecting mirror STM. In the example of the 1 the further semi-transparent or partially reflecting mirror STM splits off part of the fluorescent radiation FL. The further semi-transparent or partially reflecting mirror STM supplies this divided fluorescent radiation FL to an exemplary first camera CM1. The first camera CM1 captures an image of the quantum dots NV1, NV2, NV3 emitting fluorescent radiation FL. In the example, the 1 the control device μC accesses the first camera CM1 and the captured image of the first camera CM1. For example, a user can access the image of the first camera CM1 via the external data bus EXTDB or another interface of the control device µC via the control computer µC and control parts of the quantum computer QC depending on the captured image of the first camera CM1. The computer core CPU of the control device µC can also, for example, query the captured image of the first camera CM1 via the control data bus SDB and then evaluate it or store it in a memory RAM, NVM or process it in some other way. For example, the computer core CPU of the control device µC can execute an image processing program. For example, the computer core CPU of the control device µC or another suitable sub-device of the quantum computer QC can determine a mechanical offset of the quantum dots NV1, NV2, NV3 relative to the optical system OS, for example by evaluating the image captured by the first camera CM1 determine and determine an offset vector. The computer core CPU of the control device µC or the other suitable sub-device of the quantum computer QC preferably corrects this determined offset of the quantum dots NV1, NV2, NV3 relative to the optical system OS. For example, the computer core CPU of the control device µC or the other suitable sub-device of the quantum computer QC can eliminate the determined offset vector by means of a translational positioning device in the X direction XT and/or a translational positioning device in the Y direction YT. For this purpose, the translational positioning device preferably shifts the substrate D with the quantum ALU from quantum dots NV1, NV2, NV3 and/or nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ in the X direction XT. Cl3 ₂ , Cl3 ₃ in the x direction in such a way that the X component of the detected offset vector preferably becomes essentially 0. For example, the control device μC can preferably control the translational positioning device XT in the X direction via the control data bus SDB by means of an X control device GDX and query operating parameters of the positioning device XT in the X direction. For this purpose, the X control device GDX for the translational positioning device XT in the X direction and the translational positioning device XT in the X direction is preferably connected to the control data bus SDB. The computer core CPU of the control device µC or the other suitable sub-device of the quantum computer QC preferably carry out a control algorithm that corresponds to a PI or PI controller or another suitable controller. Furthermore, the translational positioning device preferably shifts the substrate D with the quantum ALU from quantum dots NV1, NV2, NV3 and/or nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ in the Y direction YT , Cl3 ₂ , Cl3 ₃ in the Y direction in such a way that the Y component of the detected offset vector preferably becomes essentially 0. For example, the control device μC can preferably control the translational positioning device YT in the Y direction via the control data bus SDB by means of a Y control device GDY for the translational positioning device YT in the Y direction and query operating parameters of the positioning device YT in the Y direction. For this purpose, the Y control device GDY for the translational positioning device YT in the Y direction is preferably connected to the control data bus SDB. The computer core CPU of the control device µC or the other suitable sub-device of the quantum computer QC preferably carry out a control algorithm that corresponds to a PI or PI controller or another suitable controller. The quantum computer QC preferably also has a device for re-focusing. For example, the optical system OS can comprise a sub-device that enables the optical system OS to be displaced in the Z direction relative to the substrate D. The computer core CPU of the control device µC can preferably control this sub-device to shift the optical system OS in the Z direction via the control data bus STB. Preferably, the computer core CPU of the control device µC can access operating parameters of this sub-device for shifting the optical system OS in the Z direction via the control data bus STB and preferably automatically focus the confocal microscope of the optical system OS. The computer core CPU of the control device µC preferably regulates the distance between the optical system OS and substrate D via the control data bus STB in a manner dependent on the captured image of the first camera CM1 using this sub-device to shift the optical system OS in the Z direction, that the focus of the captured images of the first camera is on the fluorescent quantum dots NV1, NV2, NV3 and remains so in the event of mechanical disturbances. If the control device µC reduces or suppresses the fluorescence radiation FL of such quantum dots NV1, NV2, NV3 too far by manipulating the quantum state of quantum dots NV1, NV2, NV3, the control device µC preferably no longer takes the fluorescence radiation FL of these quantum dots NV1, NV2, NV3 into account the duration of this state of these quantum dots NV1, NV2, NV3 when controlling the position of the substrate D relative to the optical system OS or when controlling the focus of the optical system OS. If the control device µC enables or increases the fluorescence radiation FL of such quantum dots NV1, NV2, NV3 to a sufficient extent by manipulating the quantum state of quantum dots NV1, NV2, NV3, the control device µC preferably takes the fluorescence radiation FL of these quantum dots NV1, NV2, NV3 into account again the duration of this state of these quantum dots NV1, NV2, NV3 when controlling the position of the substrate D relative to the optical system OS or when controlling the focus of the optical system OS. The proposed quantum computer QC therefore preferably comprises one or more control loops for stabilizing the spatial position of the quantum dots NV1, NV2, NV3 and/or nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ relative to the focus point of the optical system OS and possibly preferably one or more control loops for stabilizing the focus of the optical system OS on the quantum dots NV1, NV2, NV3 and/or the nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the substrate D.

If necessary, the control device µC regulates the light source LD and/or the light source driver LDRV depending on the captured image of the first camera CM1 using a light source control program. The light source control program is preferably a hardware program that the control device μC or another computer unit of the quantum computer QC continuously executes. For this purpose, the light source driver LDRV is preferably connected to the control data bus SDB. The computer core CPU can then control the light source driver LDRV via this control data bus STB and preferably query its operating parameters. It is conceivable that the proposed quantum computer QC includes an optical monitoring device within the light source LD and/or within the light source driver LDRV, for example a monitor photodiode with a device associated with this monitor photodiode for evaluating the measured values of the monitor diode, which determines the intensity of the emission of the pump radiation LB the light source LD is monitored and its parameters recorded. The computer core CPU of the control device µC can then preferably read out these recorded parameters via the control data bus SDB. The control device µC and/or said optical monitoring device of the light source LD and/or the light source driver LDRV and/or another sub-device of the deployable quantum computer QC can then control the intensity of the emission of the pump radiation LB of the light source LD, for example depending on the value of the transmission signal S5 or another parameter specified by you.

The photodetector PD detects the fluorescence radiation FL of the quantum dots NV1, NV2, NV3. The photodetector PD converts the detected fluorescence radiation FL into a receiver output signal S0. An amplifier V preferably amplifies and/or filters the receiver output signal S0. The amplifier V preferably amplifies and/or filters the receiver output signal SO depending on the transmission signal S5. The amplifier V preferably comprises one or more analog-to-digital converters. The computer core CPU of the control device µC can preferably query values of these analog-to-digital converters via the control data bus SDB. Preferably, an analog-to-digital converter ADCV of the amplifier, in cooperation with an internal amplifier IVV of the amplifier V, converts the receiver output signal S0 into measured values of sample values of the receiver output signal S0. For this purpose, the amplifier V is preferably connected to the control data bus SDB. The computer core CPU of the control device µC can preferably set and/or query operating parameters of the amplifier V via the control data bus SDB. These operating parameters can be, for example, the gain and/or filter parameters of a filtering that the amplifier V carries out.

Microwave control MW/RF-AWFG, mWA

The deployable quantum computer QC according to the proposal preferably comprises one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . For example, such a device MW/RF-AWFG, mWA can be used to generate an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₁ , Cl3 ₃ one or more microwave/radio frequency generators with preferably freely selectable waveform MW/RF-AWFG and one or more antennas mWA connected to them via one or more waveguides. These antennas mWA then generate said electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 1 , Cl2 ₂ , _{Cl2 3 ,} Cl3 ₁ , Cl3 _Z , Cl3 ₃ . A simple wire can already serve as an antenna mWA if the quantum dots NV1, NV2, NV3 are arranged at a sufficiently small distance from the wire. The said electromagnetic wave field depends on the respective location of the quantum dots NV1, NV2, NV3 and/or on the respective location of the nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ depends on the output signals of the one or more microwave/radio frequency generators, each preferably having a freely selectable waveform MW/RF-AWFG. The control device µC preferably controls the one or more devices MW/RF-AWFG, mWA via the control data bus SDB for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ . Cl3 ₂ , Cl3 ₃ . The transmission signal S5 preferably synchronizes the generation of the electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ by the one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . For example, the transmission signal S5 can generate the electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ through the one or more MW/RF devices AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ synchronize with the light source driver LDRV and thus with the emission of the pump radiation LB of the light source LD.

Control device µC

The deployable quantum computer QC preferably comprises the already mentioned control device μC with the computer core CPU. The control device μC is preferably a conventional digital computer in Von Neumann or Harvard architecture. The control device µC preferably comprises a computer core CPU and preferably one or more data and program memories RAM NVM. For example, it can be an ARM controller.

For example, the computer core CPU can be an ARM Cortex-A78AE for safety-critical applications. The ARM Cortex-A78AE is characterized by including supporting device parts and functions to meet ISO 26262 ASIL Band ASIL D security requirements. The document presented here therefore proposes, in certain cases, to provide a computer core CPU which supports device parts and functions to meet the ISO 26262 ASIL Band ASIL D safety requirements or functionally equivalent standards such as IEC 61508 and/or IEC 62061:2021, EN 61511, EN 50129, EN 62304, US RTCA DO-178B, US RTCA DO-254, EUROCAE ED-12B. The data and program memory RAM NVM or the multiple data and program memories RAM NVM can be designed in whole or in part as a non-volatile memory NVM and/or in whole or in part as a volatile memory RAM. The data and program memory of the control device µC can be read-only in whole or in part and can be read/write in whole or in part. The data and program memory RAM NVM can include, for example, a RAM, an SRAM, a DRAM, a ROM, an EEPROM, a PROM, a flash memory and/or functionally equivalent memories. The control device µC can include a bootstrap device for loading the start program into the data and program memory. The data and program memory RAM NVM of the control device µC can include a BIOS. The data and program memory RAM NVM of the control device µC can comprise a data memory and/or a program memory. The computer core CPU of the control device µC can include a data interface DBIF for communication with other computer systems, in particular a higher-level central control unit ZSE, and with user interfaces. This data interface DBIF can be wired and/or wireless. The document presented here refers to the relevant literature on data networks.

Control tasks of the control device µC

The control device µC of the proposed deployable quantum computer QC preferably also controls the intensity and modulation of the pump radiation LB and intensity modulation of the light source LD by means of its computer core µC. For this purpose, for example, the computer core CPU of the control device μC can control the time course of the intensity of the pump radiation LB emitted by the light source LD. The time course of the intensity of the pump radiation LB from the light source LD is preferably pulse-modulated. The computer core CPU of the control device µC controls the light source LED using the waveform generator WFG via the light source driver LDRV. The computer core CPU of the control device µC preferably controls the intensity l _p and/or the temporal position t _sp of the pulses and/or the temporal duration t _dp of the pulses of the pulsed pump radiation LB of the light source LD. The computer core CPU of the control device µC of the deployable quantum computer QC can thus determine the states of the quantum dots via this intensity I _p of the pulses of the pump radiation LB and via the temporal position t _sp of the pulses of the pump radiation LB and via the temporal duration t _dp of the pulses of the pump radiation LB NV1, NV2, NV3 of the proposed deployable quantum computer affect QC. Therefore, via this intensity I _p of the pulses of the pump radiation LB and via the temporal position t _sp of the pulses of the pump radiation LB and via the temporal duration t _dp of the pulses of the pump radiation LB, the computer core CPU of the control device µC of the deployable quantum computer QC can determine the states of Couple quantum dots NV1, NV2, NV3 of the quantum dots with each other. The device synchronizes these pulses of the pump radiation LB, for example by means of the computer core CPU of the control device µC and/or by means of suitable synchronizations and/or by means of synchronization signals with microwave and/or signals possibly generated by the microwave and/or radio wave frequency generator MW/RF-AWFG Radio signals for controlling the quantum dots NV1, NV2, NV3 and/or nuclear _quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 1, Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . Such a synchronization signal can be the transmission signal S5. These microwave and/or radio signals generated by the microwave and/or radio wave frequency generator MW/RF-AWFG also influence the quantum dots NV1, NV2, NV3 depending on the state of the quantum dots NV1, NV2, NV3. About such influences on the states of the quantum dots NV1, NV2, NV3 of the proposed deployable quantum computer QC, the computer core CPU of the control device µC can typically also influence the states of the nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ and, if necessary, the states of nuclear quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ with states of quantum dots NV1, NV2, NV3. Via such influences on the states of the quantum dots NV1, NV2, NV3 of the proposed deployable quantum computer QC, the computer core CPU of the control device µC can typically also influence the states of the nuclear core quantum dots Cl1, Cl2, CI3 and, if necessary, the states of the nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ couple with each other.

Said computer core CPU of the control device µC preferably controls the one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots _Cl11 , _Cl12 , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . These one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ preferably generate one or more possibly overlapping electromagnetic fields at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the nuclear core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . These electromagnetic fields are preferably designed so that they have a suitable frequency, in particular a microwave and/or radio wave frequency, f _HF , which is typically modulated with a time envelope curve in pulse form. The generation of the pulses of these pulsed electromagnetic fields with microwave and/or radio wave frequency f _HF is preferably synchronized in time with the generation of the pulses of the pump radiation LB of the light source LED, for example via the transmission signal S5. Such a pulse of these pulsed electromagnetic fields with microwave and/or radio wave frequency f _HF preferably begins at a pulse start time t _spHF relative to the reference time t _0HF and preferably has a pulse duration t _dHF . The said computer core CPU of the control device µC preferably controls both the one or more devices MW/RF-AWFG for generating the said electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the nuclear core quantum dots Cl1 ₁ . Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . The said computer core CPU of the control device µC preferably sets the frequency of the electromagnetic field f _HF , which the one or more devices MW/RF-AWFG use to generate an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location the core quantum dots Cl1 ₁ . Generate Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . The said computer core CPU of the control device µC preferably also provides a pulse start time t _spHF relative to the reference time t _0HF and possibly a pulse duration t _dHF of a temporal envelope curve of the radiation of an electromagnetic field by the one or more devices MW/RF-AWFG for generation of an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ in pulse form. In addition, said computer core CPU of the control device µC also preferably sets the amplitude I _pHF of this pulse that these devices MW/RF-AWFG, mWA generate.

In addition, the computer core CPU of the control device µC controls, if necessary, other functions of the deployable quantum computer QC and its sub-devices and methods. The quantum dots NV1, NV2, NV3 and the pairs of two quantum dots and the pairs of one quantum dot and one nuclear core quantum dot typically have different resonance frequencies f _HF . The cause is, firstly, the different spatial distances between the quantum dots within the different pairs of two quantum dots and, secondly, the different spatial distances within the different pairs of one quantum dot and a nuclear core quantum dot assigned to this quantum dot. Preferably, the computer core CPU of the control device µC measures these resonance frequencies f _HF at the start of operation and/or while still in the production facility in a test run or trial operation. To do this, use the means described above. At this point the document presented here expressly refers to the document again DE 10 2020 125 189 A1 . The computer core CPU of the control device µC preferably stores the resonance frequency values determined in this way in a memory NVM of the control device µC as stored resonance frequencies. This memory is preferably a non-volatile memory NVM. This has the advantage that this determination of the resonance frequencies through a scanning process with a typically step-by-step tuning of the frequency f _HF is then necessary less frequently and is not necessary every time the quantum computer QC is restarted. During operation, the computer core CPU of the control device µC uses these resonance frequencies stored in the memory NVM of the control device µC, in order to adjust the frequency f _HF of the electromagnetic field to be generated so that one or more devices MW/RF-AWFG, mWA for generating an electromagnetic field specifically control the state of a very specific quantum dot and/or specifically the state of a very specific pair of quantum dots and /or a very specific pair of a quantum dot and a core quantum dot can specifically influence the states of a very specific group of quantum dots. At this point the document presented here expressly refers to the document again DE 10 2020 125 189 A1 .

The computer core CPU of the control device µC can preferably control the light source driver LDRV via the internal data interface MDBIF and the control data bus SDB and read out operating parameters of the light source driver LDRV, such as internal temperatures, internal supply voltages, etc.

The computer core CPU of the control device µC can preferably control the light source LD via the internal data interface MDBIF and the control data bus SDB and read out operating parameters of the light source LD, such as temperature, light emission intensity, etc.

The computer core CPU of the control device µC can preferably control the waveform generator WFG and read out operating parameters of the waveform generator WFG via the internal data interface MDBIF and the control data bus SDB.

The computer core CPU of the control device µC can preferably control the amplifier V via the internal data interface MDBIF and the control data bus SDB and read out operating parameters of the amplifier V, such as gains and / or filter parameters.

The computer core CPU of the control device µC can preferably record and read out the measured values of the receiver output signal SO of the photodetector PD, which are amplified and filtered by the analog-to-digital converter ADCV of the amplifier V and by the amplifier V, via the internal data interface MDBIF and the control data bus SDB. If possible, the computer core CPU of the control device µC can preferably configure the photodetector PD via the internal data interface MDBIF and, if necessary, read out further operating parameters, such as a bias voltage or a temperature, or set the bias voltage.

The computer core CPU of the control device µC can preferably configure and read out the first camera CM1 via the internal data interface MDBIF and the control data bus SDB and a first camera interface CIF. The first camera CM1 preferably captures an image of the substrate D. The first camera CM1 preferably captures an image of the distribution of the fluorescence radiation FL of the substrate D and preferably transmits this image to the computer core CPU of the control device μC. The first camera CM1 preferably captures an image of the distribution of the fluorescence radiation FL of the quantum dots NV1, NV2, NV3 of the substrate D and preferably transmits this image to the computer core CPU of the control device µC. The computer core CPU of the control device µC can thus control the first camera CM1 and read out operating parameters and data from the camera CM1.

The computer core CPU of the control device µC can preferably control the X control device GDX for the translational positioning device XT in the

The computer core CPU of the control device µC can preferably control the Y control device GDY for the translational positioning device YT in the Y direction via the internal data interface MDBIF and the control data bus SDB and read out and, if necessary, adapt operating parameters of the Y control device GDY.

The computer core CPU of the control device µC can preferably control the translational positioning device XT in the X direction via the internal data interface MDBIF and the control data bus SDB and via the

The computer core CPU of the control device µC can preferably control the translational positioning device YT in the Y direction via the internal data interface MDBIF and the control data bus SDB and via the Y control device GDY and read out and, if necessary, adapt operating parameters of the translational positioning device YT in the Y direction.

The computer core CPU of the control device µC preferably detects the position of the substrate D relative to the optical system OS. The computer core CPU of the control device µC can, for example and preferably via the internal data interface MDBIF and the control data bus SDB and via the first camera interface CIF and the first camera CIM1 preferably detect this position of the substrate D relative to the optical system OS and changes in this position of the substrate D relative to the optical system OS by means of the Y control device GDY and the translational positioning device YT in the Y direction and by means of the X control device GDX and the translational positioning device XT in the X direction so that these corrections reverse these changes in this position of the substrate D relative to the optical system OS.

The computer core CPU of the control device µC can preferably read out and, if necessary, configure a temperature sensor ST via the internal data interface MDBIF and the control data bus SDB.

The computer core CPU of the control device µC can preferably reconfigure or operate differently one or more device parts of the deployable quantum computer QC via the internal data interface MDBIF and the control data bus SDB depending on the temperature detected with the temperature sensor ST. In particular, the computer core CPU of the control device µC can put one or more fans of the quantum computer QC or functionally equivalent cooling devices such as water or oil coolers with corresponding coolant circuits into operation or change their operating parameters so that the temperature detected by the temperature sensor TS remains in a predetermined temperature range. The proposed quantum computer QC can have one or more temperature sensors TS and one or more coolant circuits and/or one or more fans. All suitable fluids can be used as coolants. Air, water and oil are particularly preferred. The cooling typically serves to dissipate waste heat from device parts of the quantum computer QC. Typically, a target temperature in the range of 0°C to 50°C is preferred. A military temperature range of -40°C to 125°C seems sensible for military applications. Instead of a cooling device, the quantum computer QC can also have a heater for air conditioning purposes, whereby the computer core CPU of the control device µC can then preferably control this heater via the internal data interface MDBIF and the control data bus SDB depending on the temperature detected by the temperature sensor ST in such a way that Inside the quantum computer QC exceeds a minimum temperature. The heating can be, for example, electrical, chemical or thermonuclear.

The computer core CPU of the control device µC preferably detects the position of the substrate D relative to the optical system OS and the position of a permanent magnet PM relative to the substrate D. The computer core CPU of the control device µC can, for example and preferably, via the internal data interface MDBIF and the control data bus SDB and via the second camera interface CIF2 and the second camera CIM2 preferably capture this position of the substrate D relative to the optical system OS and the position of a permanent magnet PM relative to the substrate D, for example in the side view.

The computer core CPU of the control device µC can preferably configure and read out the second camera CM2 via the internal data interface MDBIF and the control data bus SDB and the second camera interface CIF2. The second camera CM2 preferably captures an image of the substrate D relative to the optical system OS and the position of a permanent magnet PM relative to the substrate D, for example in the side view. For this purpose, a lamp LM with a lamp preferably illuminates the area that the second camera CM2 is intended to capture. The second camera CM2 preferably captures this image and preferably transmits this image to the computer core CPU of the control device μC. The computer core CPU of the control device µC can thus control the second camera CM2 and read out operating parameters and data of the second camera CM2. This second camera CM2 makes it possible to remotely observe and check the positioning process and the positioning of the substrate D relative to the optical system OS by means of the translational positioning device XT in the X direction and the translational positioning device YT in the Y direction and, if necessary, the positioning process and to observe and check the positioning of the substrate D relative to a permanent magnet PM by means of the positioning device PV of this permanent magnet PM, without having to check the housing of the quantum computer QC. The second camera CM2 preferably transmits the image of the observed image area via the second camera interface CIF2, the control data bus SDB, the internal data interface MDBIF, the internal data bus INTDB of the control device µC, the computer core CPU of the control device µC, the external data interface DBIF of the control device µC and the external data bus EXTDB to a higher-level control unit ZSE or another computer that has a suitable human-machine interface. This human-machine interface can have a screen and a keyboard or the like, so that an operator of the quantum computer QC can make inputs here for controlling device parts of the quantum computer QC or the quantum computer QC as a whole. This or another human-machine interface can be used to display calculation results of the quantum computer QC and/or status messages of the quantum computer QC, in particular the computer core CPU of the control device µC and/or operating parameters and/or status messages of device parts of the quantum computer QC. In particular, the human-machine interface can display images and/or video sequences of the first camera CM1 and/or the second camera CM2. These images and/or video sequences can be previously processed for display by the computer core CPU of the control device µC of the quantum computer QC or a computer that is connected to the deployable quantum computer QC via the external data bus EXTDB. The computer can be a central control unit ZSE. For example, it can be false-color images, image sections and distorted images and videos or the like.

The first camera CM1 and/or the second camera CM2 do not necessarily need to be RGB cameras. Rather, they can also be sensitive to radiation that is not visible to humans. The first camera CM1 and/or the second camera CM2 can also be multispectral cameras in order, for example, to be able to optimally observe the fluorescence radiation FL of the quantum dots NV1, NV2, NV3. The first camera CM1 preferably includes imaging optics and an imaging photodetector circuit, for example a CCD sensor IC, and camera evaluation electronics that are coupled to the first camera interface CIF. The second camera CM2 preferably comprises a second imaging optics and a second imaging photodetector circuit, for example a second CCD sensor IC, and a second camera evaluation electronics which is coupled to the second camera interface CIF2.

The computer core CPU of the control device µC can preferably control a control device PVC for a positioning device PV of the permanent magnet PM via the internal data interface MDBIF and the control data bus SDB and read out and, if necessary, modify operating parameters of the control device PVC for a positioning device PV of the permanent magnet PM.

For example, the computer core CPU of the control device µC can preferably detect changes in the position of the substrate D relative to the optical system OS and the position of a permanent magnet PM relative to the substrate D, for example in the side view, via the internal data interface MDBIF and the control data bus SDB, and such changes in the position of the Rebalance the permanent magnet PM relative to the substrate D using a positioning device PV of the permanent magnet PV. For this purpose, the computer core CPU of the control device µC preferably uses the control device PVC for a positioning device PV of the permanent magnet PM. The computer core CPU of the control device µC can thereby preferably control the positioning device PV of the permanent magnet PM via the internal data interface MDBIF and the control data bus SDB by means of which the control device PVC and read out and, if necessary, modify operating parameters of the positioning device PV. In particular, the computer core CPU of the control device μC can, for example, preferably control and change the position of the permanent magnet PM via the internal data interface MDBIF and the control data bus SDB by means of the positioning device PV. Preferably, the computer core CPU of the control device µC can detect changes in the position of the permanent magnet PM relative to the substrate D using the second camera CM2 and compensate for them again using the positioning device PV.

The proposed quantum computer QC thus comprises first means (CM1, CM2) for detecting changes in the arrangement of device parts (OS, D, PM) relative to one another, and second means (XT, YT, PV) for undoing the detected changes. The first means can also include functionally equivalent sensors, in particular position sensors. The second means can also include other functionally equivalent actuators.

The computer core CPU of the control device µC can, for example, preferably control a microwave and/or radio wave frequency generator MW/RF-AWFG via the internal data interface MDBIF and the control data bus SDB to generate largely freely definable waveforms (English: arbitrary wave form generator) and its Read operating parameters and adjust if necessary. In particular, for example, the computer core CPU of the control device µC can preferably program or set the generated waveforms of the microwave and / or radio wave frequency generator MW / RF-AWFG via the internal data interface MDBIF and the control data bus SDB or read out the set waveform.

The computer core CPU of the control device µC can, for example, preferably set and configure the microwave and/or radio wave antenna mWA via the internal data interface MDBIF and the control data bus SDB and/or read out such a configuration of the microwave and/or radio wave antenna mWA. The microwave and/or radio wave frequency generator MW/RF-AWFG typically controls the microwave and/or radio wave antenna mWA with the waveforms of the microwave and/or radio wave frequency generator MW/RF-AWFG generated by the microwave and/or radio wave frequency generator MW/RF-AWFG at. The microwave and/or radio wave antenna mWA irradiates the substrate D with the quantum dots NV1, NV2, NV3 with the electromagnetic radiation corresponding to waveforms of the microwave and/or radio wave frequency generator MW/RF-AWFG generated by the microwave and/or radio wave frequency generator MW/RF-AWFG.

As a result, the electromagnetic radiation manipulates the quantum state of the quantum dots NV1, NV2, NV3 and the core quantum dots Cl1 ₁ in accordance with the waveforms of the microwave and/or radio wave frequency generator MW/RF-AWFG generated by the microwave and/or radio wave frequency generator MW/RF-AWFG. Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ in the substrate D. This allows the computer core CPU of the control device µC to control the quantum state of the quantum dots NV1, for example via the internal data interface MDBIF and the control data bus SDB , NV2, NV3 and the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 1 , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , _{Cl3 2 ,} Cl3 ₃ in the substrate D. The computer core CPU of the control device µC can typically determine the quantum state of the quantum dots NV1, NV2, NV3 and the core quantum dots Cl1 ₁ , Cl1 via the internal data interface MDBIF and the control data bus SDB using the waveform generator WFG and the light source driver LDRV and the light source LD but also in a different way ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ in substrate D.

The computer core CPU of the control device µC can, for example, preferably via the internal data interface MDBIF and the control data bus SDB a cooling device KV of the substrate D and possibly in the 1 Control auxiliary devices, not shown, of the cooling device KV of the substrate D and record and read out their status information. The auxiliary device of the cooling device KV of the substrate D can, for example, be a so-called closed loop helium gas cooling system HeCLCS that uses helium as a coolant. The computer core CPU of the control device µC can, for example, preferably control the closed loop helium gas cooling system HeCLCS via the internal data interface MDBIF and the control data bus SDB. For example, this coolant can flow through a cooling surface as a cooling device KV, with the substrate D being attached in a thermally conductive manner on the surface of the cooling surface serving as a cooling device KV and thereby the substrate is cooled by the closed loop helium gas cooling system HeCLCS. Preferably, the translational positioning device XT in the X direction and the translational positioning device YT in the Y direction position the composite of the cooling device KV and substrate D.

The computer core CPU of the control device µC can, for example, preferably control a charging device LDV via the internal data interface MDBIF and the control data bus SDB and read out operating parameters and data from the charging device LDV. Such an operating parameter can be, for example, the voltage value of the mains voltage of the electrical supply network that supplies the charging device LDV with electrical energy.

The computer core CPU of the control device µC can, for example, preferably control a separating device TS via the internal data interface MDBIF and the control data bus SDB and read out operating parameters and data from the separating device TS. For example, the computer core CPU of the control device µC can separate the outputs of the charging device LDV from the first energy reserve BENG and / or the second energy reserve BENG2, so that firstly it no longer charges the first energy reserve BENG and / or the second energy reserve BENG2 with electrical energy and secondly Secondly, the remaining device parts of the quantum computer are not disturbed or are only disturbed to a much lesser extent. For example, the computer core CPU of the control device µC can connect the outputs of the charging device LDV to the first energy reserve BENG and/or to the second energy reserve BENG2, so that it charges the first energy reserve BENG and/or the second energy reserve BENG2 with electrical energy.

The computer core CPU of the control device µC can, for example, preferably control the first energy reserve BENG and/or read out operating parameters and data from the first energy reserve BENG via the internal data interface MDBIF and the control data bus SDB. For example, the first energy reserve BENG can include several submodules that the computer core CPU of the control device µC monitors. For example, the computer core CPU of the control device µC can detect the temperature of these sub-modules and/or the pressure in these sub-modules and/or the state of charge of these sub-modules. For this purpose, the first energy reserve BENG preferably comprises suitable sensors, the values of which the computer core CPU of the control device µC can detect. In the event of an error, the computer core CPU of the control device µC can detect this error in the recorded parameters of these sub-modules and switch faulty sub-modules out of the group and bridge the resulting gap. For this purpose, the first energy reserve BENG preferably comprises suitable switches and/or changeover switches, the switching state of which can be influenced by the computer core CPU of the control device μC.

In this way, the computer core CPU of the control device μC can preferably influence the energy supply of a first energy processing device SRG.

The computer core CPU of the control device µC can, for example, preferably control the first energy processing device SRG via the internal data interface MDBIF and the control data bus SDB and / or record and read out operating parameters and data of the first energy processing device SRG. Typically, the computer core CPU of the control device μC can monitor and control the energy supply to the remaining device parts of the quantum computer QC.

If DMA accesses of the remaining device parts of the quantum computer QC are permitted, these can, for example, preferably via the internal data interface MDBIF and the control data bus SDB by means of a DMA access to the control device µC and/or the memory RAM, NVM of the control device µC and/or the the computer core CPU and/or the control device µC and the data interface DBIF and the external data bus EXTDB access devices outside the quantum computer QC.

The possibly existing internal control computers of device parts of the quantum computer QC can, for example, preferably communicate with devices outside the quantum computer QC via the control device μC and the data interface DBIF and the external data bus EXTDB and exchange data with these external devices. Such external devices can be, for example, control devices of a motor vehicle or the like. In particular, data exchange with the Internet or a comparable data network with a large number of computer systems is conceivable. These computer systems can include, for example, a deployable central control unit ZSE of a deployable quantum computer system QUSYS, part of which can be the deployable quantum computer QC.

The computer core CPU of the control device µC can write data to and read the volatile memory RAM of the control device µC. Typically, the data content of the volatile memory RAM includes program data and/or operating data and/or program instructions.

The computer core CPU of the control device µC can read the data of the non-volatile memory NVM of the control device µC. The non-volatile memory NVM of the control device µC preferably comprises a writable non-volatile memory such as a flash memory. Typically, the data content of the non-volatile memory NVM includes program data and/or operational data and/or program instructions. The data content of a non-volatile and writable memory NVM preferably includes the parameters of the resonance frequencies for driving the core quantum bits Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 _Z , Cl3 ₃ .

The computer core CPU of the control device µC can, for example, read the memory RAM, NVM of the control device µC and/or write data to it.

The computer core CPU of the control device µC can preferably access a higher-level computer system, for example a central control unit ZSE and/or the control devices of other quantum computers QC1 to QC16, via the data interface DBIF and the external data bus EXTDB.

The computer core CPU of the control device µC can access the control data bus SDB via the internal data interface MDBIF and other device parts of the deployable quantum computer QC via this control data bus SDB.

The computer core CPU of the control device µC can, for example, preferably control the light source driver LDRV and/or read out operating parameters and data of the light source driver LDRV via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, the light intensity and other adjustable operating parameters. The data that the computer core CPU of the control device µC can read out from the light source driver LDRV via the internal data interface MDBIF and the control data bus SDB can include, for example, current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, this allows the computer core CPU of the control device µC to monitor and control the light source driver LDRV of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the waveform generator WFG and/or read out operating parameters and data from the waveform generator WFG via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, the data of the waveform to be generated of the transmission signal S5 of the waveform generator WFG and/or the speed/frequency of the generation of the thus specified waveform of the generated transmission signal S5 of the waveform generator WFG and other adjustable operating parameters of the waveform generator WFG. The data that the computer core CPU of the control device µC can read out from the waveform generator WFG via the internal data interface MDBIF and the control data bus SDB for example, current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, the computer core CPU of the control device μC can monitor and control the waveform generator WFG of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the amplifier V and / or read out operating parameters and data of the amplifier V via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, the gain and/or filter parameters of the amplifier V and other adjustable operating parameters of the amplifier V. The data that the computer core CPU of the control device µC can read from the amplifier V via the internal data interface MDBIF and the control data bus SDB can include, for example, internal current strengths, internal values of electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, the computer core CPU of the control device µC can monitor and control the amplifier V of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the photodetector PD and/or read out operating parameters and data from the photodetector PD via the internal data interface MDBIF and the control data bus SDB. The control data can be, for example, the gain and/or filter parameters of a control circuit that may be present and integrated into the photodetector PD, which controls the actual photon-sensitive element of the photodetector PD and detects the values relevant for the detection of photons and converts them into a readable signal. The data that the computer core CPU of the control device µC can read from the photodetector PD via the internal data interface MDBIF and the control data bus SDB can include, for example, internal current strengths, internal values of electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, the computer core CPU of the control device µC can monitor and control the photodetector PD of the quantum computer QC. In the simplest case, it can also be a completely passive photodetector PD without any intelligence, which only transmits an analog output signal to the amplifier V.

The computer core CPU of the control device µC can, for example, preferably control the first camera CM1 and/or read out operating parameters and data of the first camera CM1 via the internal data interface MDBIF and the control data bus SDB and a first camera interface CIF. The control data can include, for example, operating parameters of the first camera CM1 such as brightness, contrast, color settings, aperture, focus, etc. of the first camera CM1 and other adjustable operating parameters of the first camera CM1. The data that the computer core CPU of the control device µC can read out from the first camera CM1 via the internal data interface MDBIF and the control data bus SDB can, for example, be the image data, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and from there include derived values. Typically, the computer core CPU of the control device µC can monitor and control the first camera CM1 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the first camera interface CIF and/or read out operating parameters and data from the first camera interface CIF via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the first camera interface CIF such as memory depth, DMA access parameters and other adjustable operating parameters of the first camera interface CIF. The data that the computer core CPU of the control device µC can read out from the first camera interface CIF via the internal data interface MDBIF and the control data bus SDB can, for example, be the image data of the first camera CM1, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived from them.

Typically, the computer core CPU of the control device µC can thereby monitor and control the first camera interface CIF of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the second camera CM2 and/or read out operating parameters and data of the second camera CM2 via the internal data interface MDBIF and the control data bus SDB and a second camera interface CIF2. The control data can include, for example, operating parameters of the second camera CM2 such as brightness, contrast, color settings, aperture, focus, etc. of the second camera CM2 and other adjustable operating parameters of the second camera CM2. The data that the computer core CPU of the control device µC via the internal Data interface MDBIF and the control data bus SDB can be read out from the second camera CM2, for example the image data, internal current strengths, internal values of electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived therefrom. Typically, the computer core CPU of the control device µC can monitor and control the second camera CM2 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the second camera interface CIF2 and/or read out operating parameters and data from the second first camera interface CIF2 via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the second camera interface CIF2 such as memory depth, DMA access parameters and other adjustable operating parameters of the second first camera interface CIF2. The data that the computer core CPU of the control device µC can read out from the second camera interface CIF2 via the internal data interface MDBIF and the control data bus SDB can, for example, be the image data of the second camera CM2, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived from them. Typically, the computer core CPU of the control device µC can monitor and control the second camera interface CIF2 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control a lamp with a lamp LM for illuminating the field of view of the second camera CM2 via the internal data interface MDBIF and the control data bus SDB and / or read out operating parameters and data of the lamp with the lamp LM. The control data can include, for example, operating parameters of the lamp with the lamp LM such as brightness, orientation and other adjustable operating parameters of the lamp with the lamp LM. The data that the computer core CPU of the control device µC can read out from the lamp with the lamp LM via the internal data interface MDBIF and the control data bus SDB can include internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom include. Typically, the computer core CPU of the control device µC can monitor and control the lamp with the lamp LM of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control one or more temperature sensors ST and/or read out operating parameters and data of the one or more temperature sensors ST via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the one or more temperature sensors ST and other adjustable operating parameters of the one or more temperature sensors ST. The data that the computer core CPU of the control device µC can read out from the one or more temperature sensors ST via the internal data interface MDBIF and the control data bus SDB can include temperature data, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and include values derived from it. Typically, this allows the computer core CPU of the control device µC to monitor and control the one or more temperature sensors ST of the quantum computer QC and the quantum computer QC itself.

The one temperature sensor ST or the multiple temperature sensors ST can include, for example, NTC resistors, PTC resistors, PN junctions, thermocouples (e.g. platinum/rhodium thermocouples) or the like and/or evaluation electronics as temperature-sensitive sensor elements.

If the quantum computer QC is to be used in hot or very cold environments, the quantum computer QC can have one or more heating devices and/or cooling devices for the quantum computer QC as a whole. If the quantum computer QC is to be used in hot or very cold environments, the computer core CPU of the control device µC can then, for example, preferably via the internal data interface MDBIF and the control data bus SDB these one or more heating devices for the quantum computer QC and / or these one or more cooling devices for the quantum computer QC as a whole and / or read out operating parameters and data of these one or more heating devices and / or cooling devices for the quantum computer QC. The control data may include, for example, operating parameters of the one or more heating devices and/or one or more cooling devices for the quantum computer QC and other adjustable operating parameters of the one or more heating devices and/or cooling devices for the quantum computer QC. The data that the computer core CPU of the control device µC via the internal data interface MDBIF and the control data bus SDB from one or more More heating devices and / or cooling devices for the quantum computer QC can read out temperature data, internal current strengths, internal values of electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, this allows the computer core CPU of the control device µC to monitor and control the one or more heating devices and/or cooling devices for the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the microwave and/or radio wave frequency generator MW/RF-AWFG via the internal data interface MDBIF and the control data bus SDB to generate largely freely definable waveforms and/or operating parameters and data of the microwave and/or radio wave frequency generator Read out MW/RF-AWFG. The control data can, for example, be operating parameters of the microwave and/or radio wave frequency generator MW/RF-AWFG, such as waveform, wave frequency, amplitude and time delay compared to a synchronization signal, such as the transmission signal S5, and other adjustable operating parameters of the microwave and/or radio wave frequency generator MW/RF -AWFG include. The data that the computer core CPU of the control device µC can read out from the microwave and/or radio wave frequency generator MW/RF-AWFG via the internal data interface MDBIF and the control data bus SDB can include internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived from them etc. include. Typically, the computer core CPU of the control device µC can thereby monitor and control the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the magnetic field sensors MSx, MSy, MSz via the internal data interface MDBIF and the control data bus SDB and via the magnetic field controllers MFSx, MFSy, MFSz and/or read out operating parameters and data from the magnetic field sensors MSx, MSy, MSz. The control data can include, for example, operating parameters of the magnetic field sensors MSx, MSy, MSz such as sensitivity, current supply and other adjustable operating parameters of the microwave and/or radio wave frequency generator MW/RF-AWFG. The data that the computer core CPU of the control device µC can read out from the magnetic field sensors MSx, MSy, MSz via the internal data interface MDBIF and the control data bus SDB can include the magnetic field measurements, internal current strengths, internal values of electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived from it etc. include. Typically, the computer core CPU of the control device µC can monitor and control the magnetic field sensors MSx, MSy, MSz of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the first magnetic field controller MFSx and/or read out operating parameters and data of the first magnetic field controller MFSx via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the first magnetic field control MFSx such as the strength of the magnetic flux density B _x to be set in the direction of the first direction, the current supply to be set to the first magnetic field generating means MGx and other adjustable operating parameters of the first magnetic field control MFSx. The data that the computer core CPU of the control device µC can read out from the first magnetic field controller MFSx via the internal data interface MDBIF and the control data bus SDB can include the magnetic field measurement values, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and those derived therefrom Values etc. include. Typically, the computer core CPU of the control device µC can thereby monitor and control the first magnetic field control MFSx of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the second magnetic field control MFSy and/or read out operating parameters and data of the second magnetic field control MFSy via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the second magnetic field control MFSy, such as the strength of the magnetic flux density B _y to be set in the direction of the second direction, the current supply to be set to the second magnetic field generating means MGy and other adjustable operating parameters of the second magnetic field control MFSy. The data that the computer core CPU of the control device µC can read out from the second magnetic field controller MFSy via the internal data interface MDBIF and the control data bus SDB can include the magnetic field measurements, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and those derived therefrom Values etc. include. Typically, the computer core CPU of the control device µC can thereby monitor and control the second magnetic field control MFSy of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the third magnetic field controller MFSz and/or read out operating parameters and data from the third magnetic field controller MFSz via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the third magnetic field control MFSz such as the strength of the magnetic flux density B _z to be set in the direction of the third direction, the current supply to be set to the third magnetic field generating means MGy and other adjustable operating parameters of the third magnetic field control MFSz. The data that the computer core CPU of the control device µC can read out from the third magnetic field controller MFSz via the internal data interface MDBIF and the control data bus SDB can include the magnetic field measurement values, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and those derived therefrom Values etc. include. Typically, the computer core CPU of the control device µC can thereby monitor and control the third magnetic field control MFSz of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the first energy processing device SRG and/or read out operating parameters and data of the first energy processing device SRG via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the first energy processing device SRG, such as the voltage values to be delivered to other device parts and maximum current intensities and other adjustable operating parameters of the first energy processing device SRG. The data that the computer core CPU of the control device µC can read out from the first energy processing device SRG via the internal data interface MDBIF and the control data bus SDB can include internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom, etc. include. Typically, the computer core CPU of the control device μC can thereby monitor and control the first energy processing device SRG of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the second energy processing device SRG2 and/or read out operating parameters and data of the second energy processing device SRG2 via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the second energy processing device SRG2, such as the voltage values to be delivered to other device parts and maximum current intensities and other adjustable operating parameters of the second energy processing device SRG2. The data that the computer core CPU of the control device µC can read out from the second energy processing device SRG2 via the internal data interface MDBIF and the control data bus SDB can include internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom, etc. include. Typically, the computer core CPU of the control device μC can thereby monitor and control the second energy processing device SRG2 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the energy reserve BENG and/or read out operating parameters and data from the energy reserve BENG via the internal data interface MDBIF and the control data bus SDB. If the energy reserve BENG has its own control and monitoring device, the computer core CPU of the control device µC can, for example, preferably send control data to this control and monitoring device of the energy reserve BENG via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the energy reserve BENG such as maximum temperatures, etc. The control and monitoring device of the BENG energy reserve preferably has means for monitoring important, in particular safety-relevant, operating parameters of the BENG energy reserve. These means can include temperature sensors, voltage and current sensors or pressure sensors for measuring the internal pressure of battery cells. The data that the computer core CPU of the control device µC can read out from the energy reserve BENG via the internal data interface MDBIF and the control data bus SDB can, for example, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived therefrom etc. include. Typically, the computer core CPU of the control device µC can monitor and control the energy reserve BENG of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the energy reserve BENG and/or read out operating parameters and data from the second energy reserve BENG2 via the internal data interface MDBIF and the control data bus SDB. If the second energy reserve BENG2 has its own control and monitoring device, the computer core can CPU of the control device µC, for example, preferably send control data to this control and monitoring device of the second energy reserve BENG2 via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the second energy reserve BENG2 such as maximum temperatures, etc. The control and monitoring device of the second energy reserve BENG2 preferably has means for monitoring important, in particular safety-relevant, operating parameters of the second energy reserve BENG2. These means can include temperature sensors, voltage and current sensors or pressure sensors for measuring the internal pressure of battery cells. The data that the computer core CPU of the control device µC can read out from the second energy reserve BENG2 via the internal data interface MDBIF and the control data bus SDB can, for example, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom, etc . include. Typically, this allows the computer core CPU of the control device µC to monitor and control the second energy reserve BENG2 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the separating device TS and/or read out operating parameters and data from the separating device TS via the internal data interface MDBIF and the control data bus SDB. If the separating device TS has its own control and monitoring device, the computer core CPU of the control device µC can, for example, preferably send control data to this control and monitoring device of the separating device TS via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the separating device TS such as closing status (connected/disconnected), maximum temperatures, etc. The control and monitoring device of the separating device TS preferably has means for monitoring important, in particular safety-relevant, operating parameters of the separating device TS. These means may include temperature sensors, voltage and current sensors. The data that the computer core CPU of the control device µC can read out from the separating device TS via the internal data interface MDBIF and the control data bus SDB can, for example, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived therefrom etc. include. Typically, the computer core CPU of the control device µC can monitor and control the separation device TS of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the charging device LDV and/or read out operating parameters and data from the charging device LDV via the internal data interface MDBIF and the control data bus SDB. If the charging device LDV has its own control and monitoring device, the computer core CPU of the control device µC can, for example, preferably send control data to this control and monitoring device of the charging device LDV via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the charging device LDV such as mains voltage of the power supply PWR of the charging device LDV, output voltages of the charging device LDV to be set, maximum temperatures, etc. The control and monitoring device of the separating device TS preferably has means for monitoring important, in particular safety-relevant, operating parameters of the loading device LDV. These means may include temperature sensors, voltage and current sensors. The data that the computer core CPU of the control device µC can read out from the charging device LDV via the internal data interface MDBIF and the control data bus SDB can, for example, be the actual mains voltage of the power supply PWR of the charging device LDV, actually set output voltages of the charging device LDV, internal current strengths, internal Values include electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived therefrom etc. Typically, the computer core CPU of the control device µC can monitor and control the charging device LDV of the quantum computer QC.

• - einen oder mehrere Werte von Betriebsspannungen von Vorrichtungsteilen des Quantencomputers QC,
• - einen oder mehrere Werte von Stromaufnahmen von Vorrichtungsteilen des Quantencomputers QC,
• - den Prozessortakt des Rechnerkerns CPU der Steuervorrichtung µC des Quantencomputers QC und/oder dessen Frequenz,
• - die Prozessortakte anderer Vorrichtungsteile des Quantencomputers QC und/oder deren Frequenz,
• - die Lichtabgabe der Lichtquelle LD des Quantencomputers QC, insbesondere die Intensität der Pumpstrahlung LB der Lichtquelle LD,
• - die Signalerzeugung des der Wellenformgenerators WFG des Quantencomputers QC,
• - die Funktionstüchtigkeit der Datenschnittstelle DBIF,
• - die Funktionstüchtigkeit der die internen Datenschnittstelle MDBIF,
• - die Funktionstüchtigkeit des Lichtquellentreibers LDRV,
• - die Funktionstüchtigkeit des Verstärkers V,
• - die Funktionstüchtigkeit der Fotodetektor PD,
• - die Temperatur mittels eines Temperatursensors ST,
• - die Funktionstüchtigkeit des Mikrowellen- und/oder Radiowellenfrequenzgenerators MW/RF-AWFG zur Erzeugung weitestgehend frei vorgebbarer Wellenformen,
• - die Funktionstüchtigkeit der Magnetfeldsensoren MSx, MSy, MSz,
• - die Funktionstüchtigkeit der Magnetfeldsteuerungen MFSx, MFSy, MFSz,
• - die Funktionstüchtigkeit der ersten Energieaufbereitungsvorrichtung SRG,
• - die Funktionstüchtigkeit der zweiten Energieaufbereitungsvorrichtung SRG2,
• - die Funktionstüchtigkeit der Energiereserve BENG,
• - die Funktionstüchtigkeit der zweiten Energiereserve BENG2,
• - die Funktionstüchtigkeit der Trennvorrichtung TS,
• - die Funktionstüchtigkeit der Ladevorrichtung LDV.
• - -die Detektionsfähigkeit von elektromagnetischer Strahlung eines Fotodetektors
• - -die bestimmungsgemäß korrekte Erzeugung elektromagnetischer Felder, insbesondere von Mikrowellenfeldern und/oder Radiowellenfeldern eine Vorrichtung des Quantencomputers QC zur Manipulation eines oder mehrerer Quantenbits QUB,
• - -den komplexen und/oder realen und/oder imaginären Leitwert einer Leitung und der Mikrowellen- und/oder Radiowellenantenne MWA, die Teil der Vorrichtung des Quantencomputers QC zur Manipulation eines oder mehrerer Quantenpunkte NV1, NV2, NV3 ist.

The deployable quantum computer QC according to the proposal preferably has a quantum computer monitoring device QUV, which monitors the quantum computer QC while the quantum computer QC executes a quantum computer program with a quantum computer program sequence, which is preferably stored in its memory RAM, NVM. The document presented here refers to the as yet unpublished German patent application DE 10 2021 110 964.7 and any subsequent registrations resulting from priority claims. This quantum computer monitoring device QUV monitors the correct quantum computer program flow of the quantum computer program of the quantum computer QC. The quantum computer monitoring device QUV preferably monitors at least the value and/or value progression one, better several and optimally all of the following operating parameters monitored:

• - one or more values of operating voltages of device parts of the quantum computer QC,
• - one or more values of current consumption of device parts of the quantum computer QC,
• - the processor clock of the computer core CPU of the control device µC of the quantum computer QC and / or its frequency,
• - the processor clocks of other device parts of the quantum computer QC and/or their frequency,
• - the light output of the light source LD of the quantum computer QC, in particular the intensity of the pump radiation LB of the light source LD,
• - the signal generation of the waveform generator WFG of the quantum computer QC,
• - the functionality of the DBIF data interface,
• - the functionality of the internal data interface MDBIF,
• - the functionality of the light source driver LDRV,
• - the functionality of the amplifier V,
• - the functionality of the photodetector PD,
• - the temperature using a temperature sensor ST,
• - the functionality of the microwave and/or radio wave frequency generator MW/RF-AWFG to generate largely freely definable waveforms,
• - the functionality of the magnetic field sensors MSx, MSy, MSz,
• - the functionality of the magnetic field controls MFSx, MFSy, MFSz,
• - the functionality of the first energy processing device SRG,
• - the functionality of the second energy processing device SRG2,
• - the functionality of the BENG energy reserve,
• - the functionality of the second energy reserve BENG2,
• - the functionality of the separating device TS,
• - the functionality of the LDV charging device.
• - -the detection capability of electromagnetic radiation of a photodetector
• - - the correct generation of electromagnetic fields, in particular microwave fields and / or radio wave fields, a device of the quantum computer QC for manipulating one or more quantum bits QUB,
• - -the complex and/or real and/or imaginary conductance of a line and the microwave and/or radio wave antenna MWA, which is part of the device of the quantum computer QC for manipulating one or more quantum dots NV1, NV2, NV3.

Quantum computer monitoring device QUV Typically, the T2 times of the quantum dots NV1, NV2, NV3 and the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 _Z , Cl3 ₃ are limited. Therefore, there are time breaks between two quantum computer calculations, during which a quantum computer monitoring device QUV of the quantum computer QC can check the functionality of the remaining quantum computer QC.

Typically, the quantum computer QC carries out its quantum computer calculations within first time periods, which are typically shorter than the T2 times of the quantum dots NV1, NV2, NV3 and the core quantum dots Cl1 ₁ . Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ are, through. The quantum computer monitoring device QUV preferably carries out tests on the remaining device parts of the quantum computer QC within second time periods. The first periods are preferably different from the second periods. A quantum computer calculation in the sense of this document includes at least one quantum operation, such as, for example, an initialization of one or more quantum dots NV1, NV2, NV3 and the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ and/or, for example, the execution of a quantum gate such as a CNOT operation or a CCNOT operation or a Hadamard gate or a π pulse or an X gate etc.

In this context, the document presented here refers to the book by Steven Prawer (editor), Igor Aharonovich (editor), “Quantum Information Processing with Diamond: Principles and Applications”, Woodhead Publishing Series in Electronic and Optical Materials, Volume 63, Woodhead Publishing , May 8, 2014, ISBN-10: 0857096567, ISBN-13: 978-0857096562.

Since the result of a quantum calculation by the quantum computer QC only with a certain Statistics provides correct results, the quantum computer monitoring device QUV collects several of the results of several similar requests from the quantum computer monitoring device QUV to the computer core CPU of the quantum computer QC transmitted in response to the remaining quantum computer QC from the computer core CPU and preferably evaluates them statistically. If the determined statistics of the results of several similar requests from the quantum computer monitoring device QUV transmitted by the computer core CPU to carry out quantum calculations to the computer core CPU of the quantum computer QC deviate from an expected statistic by more than x*σ, the quantum computer monitoring device QUV typically concludes that there is an error in the Quantum Computer QC. Here σ represents the standard deviation of the statistical distribution of the expected response value. Preferably, x is between 1 and 4. Depending on the type of error when executing a quantum computer program, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures.

In the simplest case, exemplary countermeasures can include, for example, resetting and reinitializing the quantum computer QC and/or device parts of the quantum computer QC and/or starting a more extensive self-test program.

A special countermeasure can, for example, also be a translational shift of the substrate D relative to the optical system OS, so that other quantum dots NV1, NV2, NV3 are connected to other core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ replaced the previously used quantum dots NV1, NV2, NV3 and core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ . In this case, a reinitialization of the quantum computer QC is unavoidable. In particular, the computer core determines CPU using the methods of DE 10 2020 007 977 B4 the resonance frequencies for driving and manipulating and entangling the other quantum dots NV1, NV2, NV3 with other core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ and preferably stores these in its non-volatile memory NVM and less preferably in its volatile memory RAM. For the translational displacement of the substrate D relative to the optical system OS, the computer core CPU preferably uses the translational positioning device XT of the substrate D in the X direction and the translational positioning device of the substrate D in the Y direction.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to carry out a predetermined quantum computer calculation after carrying out a quantum computer calculation in the first period of time and to transmit the result of the quantum computer calculation back to the quantum computer monitoring device QUV. If the deployable quantum computer QC does not respond within a predetermined time window to the quantum computer monitoring device QUV of the deployable quantum computer QC, there may be an error. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU the control device µC of the deployable quantum computer QC with values that lie within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the execution as incorrect. For this purpose, the quantum computer monitoring device QUV of the deployable quantum computer QC preferably keeps statistical records. If the statistical distribution of the contents of the responses of the computer core CPU of the control device μC of the deployable quantum computer QC does not correspond to an expected statistical distribution, the quantum computer monitoring device QUV of the deployable quantum computer QC preferably also concludes that there is an error. Depending on the type of error, the quantum computer monitoring device QUV of the deployable quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the deployable quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

Such a test typically also checks the correct generation of electromagnetic fields, in particular microwave fields and / or radio wave fields, by a device of the deployable quantum computer QC for manipulating one or more quantum dots NV1, NV2, NV3 in the sense of the ones presented here The following documents are, for example, the waveform generator, the light source driver LDRV, the light source LD, the microwave and/or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms (Arbitrary Wave Form Generator) and the microwave and/or or radio wave antenna mWA as well as in the broadest sense the magnetic field generating means MGx, MGy, MGz and the associated magnetic field controls MFSx, MFSy, MFSz as well as the magnetic field sensors MSx, MSy, MSz. Such a test also partly tests the complex and/or real and/or imaginary conductance of a line and the microwave and/or radio wave antenna MWA, which is part of the device of the quantum computer QC for manipulating one or more quantum dots NV1, NV2, NV3 .

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a query message via the internal data bus INTDB to query one or more values of operating voltages of device parts of the quantum computer QC in the second time periods after carrying out a quantum computer calculation in the second time periods and pass it on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to, after carrying out a quantum computer calculation in the first periods, one or more values of current consumption from device parts of the quantum computer QC, from other device parts of the quantum computer QC in the second periods of time and pass it on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

The clock generator OSZ of the computer core CPU of the control device µC of the quantum computer QC typically supplies the computer core CPU of the control device µC of the quantum computer QC with a clock for operating the computer core CPU of the control device µC of the quantum computer QC. The clock generator OSZ of the computer core CPU of the control device μC of the quantum computer QC can also preferably supply further digital circuits and device parts of the quantum computer QC with a clock for operating these digital circuits and device parts of the quantum computer QC.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the processor clock of the computer core CPU of the control device μC of the quantum computer QC and/or its frequency, in particular during or after carrying out a quantum computer calculation in the first time periods and/or the second time period . If an error occurs, such as an incorrect processor clock frequency or a processor clock jitter, the quantum computer monitoring device QUV of the quantum computer QC evaluates the processor clock as incorrect. Thus, the quantum computer monitoring device QUV of the quantum computer QC preferably monitors the clock OSZ of the computer core CPU of the control device μC of the quantum computer QC.

Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible maximum frequency value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

If necessary, the quantum computer monitoring device QUV of the quantum computer QC has its own monitoring clock generation ÜOSZ. Preferably, the monitoring clock generation ÜOSZ of the quantum computer monitoring device QUV of the quantum computer QC typically supplies the quantum computer monitoring device QUV of the quantum computer QC with a clock for operating the quantum computer monitoring device QUV of the quantum computer QC.

For example, the computer core CPU of the quantum computer QC can check the processor clock of the quantum computer monitoring device QUV of the quantum computer QC and/or its frequency and/or the monitoring clock generation ÜOSZ, in particular after carrying out a quantum computer calculation in the second time periods. If an error occurs, such as an incorrect processor clock frequency or a processor clock jitter, the computer core CPU of the quantum computer QC evaluates the processor clock of the quantum computer monitoring device QUV of the quantum computer QC as incorrect. The computer core CPU of the quantum computer QC thus preferably monitors the monitoring clock generation ÜOSZ of the quantum computer monitoring device QUV of the quantum computer QC.

Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

The quantum computer monitoring device QUV preferably has a separate energy supply with preferably a further energy reserve and its own energy processing device. Preferably, the charging device LDV or another additional charging device feeds this additional energy processing device and/or the charging supplies this additional energy reserve. These optional device parts, the further energy reserve, the further energy processing device and the further charging device and possibly a further separation device of the quantum computer monitoring device QUV of the quantum computer QC and their connecting lines are in the 1 no longer shown for better clarity.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the processor input of other device parts of the quantum computer QC and/or their frequency, in particular during or after the execution of a quantum computer calculation in the first time periods and/or the second time period. If an error occurs, such as an incorrect processor clock frequency or processor clock jitter, the quantum computer monitoring device QUV of the quantum computer QC evaluates the relevant processor clock as incorrect. The quantum computer monitoring device QUV of the quantum computer QC thus preferably also monitors the clocks of other device parts of the quantum computer QC. These clocks of other device parts of the quantum computer QC are in the 1 Also not shown for better clarity. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error in the other processor clocks of other device parts of the quantum computer QC exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the light output of the light source LD of the quantum computer QC, in particular after performing a quantum computer calculation in the second periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to obtain one or more values of monitor diodes of the light source LD of the quantum after performing a quantum computer calculation in the first periods to query computers QC in the second time periods and to pass it on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check, in particular after carrying out a quantum computer calculation in the second periods, the control of the light source LD of the quantum computer QC by the light source driver LDRV and the functionality of the light source driver LDRV. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to, after performing a quantum computer calculation in the first periods by means of an analog-to-digital converter or the like, one or more values of the operating parameters of the light source driver LDRV and/or or to record one or more values of the control signals of the light source driver LDRV for the light source LD of the quantum computer QC in the second time periods and to pass them on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the generation of the transmission signal S5 by the waveform generator WFG of the quantum computer QC, in particular after carrying out a quantum computer calculation in the second periods. For this purpose, the quantum computer QC and/or the waveform generator WFG can include a measuring device, for example a digital storage oscilloscope or a similar signal detection device, that records the time course of the transmission signal S5. For example, it can be an analog-to-digital converter that records this signal curve of the transmission signal S5. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to cause the waveform generator WFG of the quantum computer QC to generate a transmission signal S5 in the second time periods after carrying out a quantum computer calculation in the first periods and by means of the Said signal detection device to record the time course of the transmission signal S5. The computer core CPU preferably evaluates the time course of the transmission signal S5 recorded in this way and transmits the result of this evaluation to the quantum computer monitoring device QUV in response to the request from the quantum computer monitoring device QUV. It is also conceivable that the computer core CPU of the quantum computer QC transmits the detected signal curve of the transmission signal S5 to the quantum computer monitoring device QUV in response to the request of the quantum computer monitoring device QUV and then the quantum computer monitoring device QUV evaluates the detected signal curve of the transmission signal S5. The response from the computer core CPU should be sent to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request is made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU the control device µC of the quantum computer QC with values that lie within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the execution as incorrect. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the generation of the output signal of the microwave and / or radio wave frequency generator MW / RF-AWFG of the quantum computer QC, in particular after carrying out a quantum computer calculation in the second periods. For this purpose, the quantum computer QC and/or the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC can include a measuring device, for example a digital storage oscilloscope or a similar signal detection device, that measures the time course of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG captured by the quantum computer QC. For example, it can be an analog-to-digital converter that records this signal curve of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to use the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC in the second periods after performing a quantum computer calculation in the first periods To generate an output signal with a specific waveform for test purposes and to record the time course of the output signal of the microwave and / or radio wave frequency generator MW / RF-AWFG of the quantum computer QC by means of said signal detection device. The quantum computer monitoring device QUV of the quantum computer QC can also cause the computer core CPU to use the request message via the internal data bus INTDB to use the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC in the second periods after performing a quantum computer calculation in the first periods To cause the generation of an output signal with a specific waveform for test purposes and to detect the amount and/or phase of the power reflected by the microwave and/or radio wave antenna MWA by means of said signal detection device and thus to the impedance of the microwave and/or radio wave antenna MWA and to close its supply line and record it. The computer core CPU preferably evaluates the time profile of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC and/or the acquired measured values and transmits the result of this evaluation to the quantum computer monitoring device QUV in response to the request of the quantum computer monitoring device QUV. It is also conceivable that the computer core CPU of the quantum computer QC transmits the detected signal curve of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC to the quantum computer monitoring device QUV in response to the request of the quantum computer monitoring device QUV and then the quantum computer monitoring device QUV the recorded signal curve of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC is evaluated. The response from the computer core CPU should be sent to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of to check the functionality of the data interface DBIF, in particular after carrying out a quantum computer calculation in the second periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to communicate via the data interface DBIF and the external data bus EXTDB with a higher-level computer system for test purposes in the second after carrying out a quantum computer calculation in the first periods time periods. The higher-level computer system can be, for example, a central control unit ZSE. The higher-level computer system preferably responds with an evaluable answer within a predetermined period of time. The computer core CPU preferably evaluates the message received from the external computer system via the data interface DBIF and the external data bus EXTDB and transmits the result of this evaluation to the quantum computer monitoring device QUV in response to the request from the quantum computer monitoring device QUV. It is also conceivable that the computer core CPU of the quantum computer QC transmits the message received from the external computer system via the data interface DBIF and the external data bus EXTDB to the quantum computer monitoring device QUV in response to the request from the quantum computer monitoring device QUV and then the quantum computer monitoring device QUV via the Data interface DBIF and the external data bus EXTDB evaluates the message received from the external computer system. The response of the computer core CPU and the higher-level computer system, for example the central control device ZSE, should preferably be sent to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the internal data interface MDBIF, in particular after carrying out a quantum computer calculation in the second periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to communicate via the internal data interface MDBIF and the control data bus SDB with an internal computer core of another device part of the quantum computer after performing a quantum computer calculation in the first periods QC to be arranged in the second periods. The internal computer core of the other device part of the quantum computer QC preferably responds with an evaluable answer within a predetermined period of time. The computer core CPU preferably evaluates the message received via the internal data interface MDBIF and the internal data bus INTDB and the control data bus SDB from the internal computer core of the other device part of the quantum computer QC and transmits the result of this evaluation to the quantum computer monitoring device QUV in response to the request of the quantum computer monitoring device QUV. It is also conceivable that the computer core CPU of the quantum computer QC sends the message received via the internal data interface MDBIF and the internal data bus INTDB and the control data bus SDB from the internal computer core of the other device part of the quantum computer QC to the quantum computer monitoring device QUV in response to the request Quantum computer monitoring device QUV is transmitted and then the quantum computer monitoring device QUV evaluates the message received via the internal data interface MDBIF and the internal data bus INTDB and the control data bus SDB from the internal computer core of the other device part of the quantum computer QC. The response of the computer core CPU and the internal computer core of the other device part of the quantum computer QC should preferably be sent to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the execution as incorrect. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the amplifier V and the functionality of the photodetector PD, in particular after carrying out a quantum computer calculation in the second periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to cause the light source LD of the quantum computer QC to emit a defined light after performing a quantum computer calculation in the first periods or a test radiation source of the quantum computer QC in the second periods cause to emit a test light emission that irradiates the photodetector PD, and / or cause the photodetector PD to generate a test signal for the amplifier V in the second time periods and query the recorded values in the amplifier V and / or operating parameters of the amplifier V and the photodetector PD to be recorded and passed on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

The computer core CPU of the control device µC of the quantum computer QC can typically control the preferably provided test radiation source of the quantum computer QC via the internal data bus interface MDBIF and the internal data bus INTDB and the control data bus SDB. Typically, the control device μC of the quantum computer QC can irradiate the photodetector PD of the quantum computer QC with an optical test signal, for example by means of an optical test radiation source, in order to ensure the functionality of the quantum computer QC. For a better overview, this test radiation source of the deployable quantum computer QC is for irradiating the photodetector PD with test radiation in the 1 not shown.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check temperatures within the quantum computer QC by means of one or more temperature sensors ST, in particular after carrying out a quantum computer calculation in the second time periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to detect one or more temperatures within the quantum computer QC by means of one or more temperature sensors ST of the quantum computer QC after carrying out a quantum computer calculation in the first periods of time and to pass on the recorded temperature measurements to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. This can already be the case in the document presented here countermeasures or other countermeasures described.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to, in particular after carrying out a quantum computer calculation in the second periods, check the functionality of the magnetic field sensors MSx, MSy, MSz and/or the functionality of the magnetic field controllers MFSx, MFSy, MFSz and/or the functionality of the Check magnetic field generating means MGx, MGy, MGz. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to perform various quantum computer calculations in the first periods by means of the magnetic field controllers MFSx, MFSy, MFSz and the magnetic field generating means MGx, MGy, MGz of the quantum computer QC to set magnetic flux densities and to record them using the magnetic field sensors MSx, MSy, MSz and to pass on the recorded measured values to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the first energy processing device SRG and/or the functionality of the second energy processing device SRG2 and/or the functionality of the further energy processing devices, in particular after carrying out a quantum computer calculation in the second time periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to set certain supply voltages after carrying out a quantum computer calculation in the first time periods using the first energy processing device SRG and / or the second energy processing device SRG2 and / or the further energy processing devices to adjust and/or modify device parts of the quantum computer QC and, for example, to use measuring devices to adjust their voltage values and/or current values and to pass on the recorded measured values to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the energy reserve BENG and/or the functionality of the second energy reserve BENG2 and/or the functionality of any further energy reserves, if any, of other device parts, in particular after carrying out a quantum computer calculation in the second time periods or already named device parts of the quantum computer QC. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB, after carrying out a quantum computer calculation in the first periods, by means of charging devices, such as the already named charging device LDV, to check the state of charge of the energy reserve BENG and / or the Functionality of the second energy reserve BENG2 and/or the radio To change the capability of further energy reserves, if necessary, of further device parts and to record the values of the respective current consumption and the voltage curve using suitable measuring devices of the quantum computer QC and thus, for example, to draw conclusions about the impedance of these energy reserves. In this case, the quantum computer monitoring device QUV of the quantum computer QC causes the computer core CPU to pass on the recorded measured values to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window using the said request message via the internal data bus INTDB. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the separation device TS of the quantum computer QC and the functionality of the loading device LDV of the quantum computer QC, in particular after carrying out a quantum computer calculation in the second periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to open the separating device TS after carrying out a quantum computer calculation in the first periods of time and to use the charging devices, such as the already mentioned charging device LDV, to check the charging status of the the energy reserve BENG and/or the functionality of the second energy reserve BENG2 and/or the functionality of any further energy reserves, if any, of other device parts and thereby to record the values of the respective current consumption and the voltage curve using suitable measuring means of the quantum computer QC and to close the separating device TS close and by means of the charging devices, such as the already named charging device LDV, the charge state of the energy reserve BENG and / or the functionality of the second energy reserve BENG2 and / or the functionality of any further energy reserves, if necessary, of other device parts to change again and thereby second values of the respective Current consumption and the voltage curve can be recorded using suitable measuring equipment from the QC quantum computer. In this case, the quantum computer monitoring device QUV of the quantum computer QC causes the computer core CPU to pass on the recorded measured values and second measured values to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window via the said request message via the internal data bus INTDB. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with first and second values that lie within expected value ranges, the quantum computer monitoring device QUV evaluates the Quantum computer QC considered the execution to be faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

Quantum computer system QSYS

If the deployable quantum computer QC according to the proposal is integrated into a quantum computer system QUSYS with a second, preferably mobile quantum computer QC2, it is advantageous if a signaling, in particular of a quantum computer calculation result, is sent from the quantum computer QC via at least one signal connection, for example an external data bus EXTDB, to the second Quantum computer QC2 and/or vice versa can be done.

The deployable quantum computer system preferably comprises QUSYS with at least two quantum computers, a first deployable quantum computer QC1 and a second deployable quantum computer QC2, with several measuring devices for recording operating variables of the Quan tencomputer system QUSYS or a device or a system. Typically, the states of the device or system depend on the quantum computer system QUSYS, whereby the first deployable quantum computer QC1 preferably carries out at least twice the same quantum computer calculation that the second deployable quantum computer QC2 carries out. The quantum computer calculation preferably includes a monitoring measure for checking the functionality of the respective deployable quantum computer QC1, QC2. The first deployable quantum computer QC1 preferably carries out the quantum computer calculation of the first deployable quantum computer QC1 independently of the implementation of the quantum computer calculation of the second deployable quantum computer QC2. This makes it possible to compare the results of the quantum computer calculations by the computer cores CPU of the control devices μC of the deployable quantum computers QC1, QC2 and/or the quantum computer monitoring devices QUV of the deployable quantum computers QC1, QC1.

Monitoring procedures

The document presented here also proposes a method for monitoring the execution of a quantum computer program that can be executed on at least one control device µC of a deployable quantum computer QC by means of a quantum computer monitoring device QUV of the quantum computer QC. The deployable quantum computer QC includes quantum dots NV1, NV2, NV3 and preferably core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and the control device µC with the computer core CPU and first means for manipulating quantum dots NV1, NV2, NV3 and, if necessary, for manipulating core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC and second means for reading out the state of quantum dots NV1, NV2, NV3 and, if applicable, core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC. The computer core CPU of the control device µC preferably controls the first means for manipulating quantum dots NV1, NV2, NV3 and possibly core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC and the second means for reading out the state of quantum dots NV1, NV2, NV3 and possibly core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the Quantum Computer QC. The quantum computer monitoring device QUV preferably triggers upon manipulation of a subset of the quantum dots and/or possibly the core quantum dots of the quantum dots NV1, NV2, NV3 and possibly core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC during the quantum computer program runtime, an exception, in particular an interruption, of the quantum computer program flow, if this manipulation was not intended. This can happen during a program jump due to interference such as cosmic radiation, which is intercepted by this.

The document presented here proposes a non-volatile memory NVM, in particular a read-only memory or a flash memory or a non-volatile memory, for the deployable quantum computer QC, in particular as part of a control unit of a vehicle. A quantum computer program is preferably stored in the non-volatile memory NVM, which can be executed on at least one computer core µC of the quantum computer QC and is suitable for carrying out the method described above.

• Auf dem mindestens einen Rechnerkern CPU der Steuervorrichtung µC soll ein Quantencomputerprogramm ablauffähig sein. Die Quantencomputerüberwachungsvorrichtung QUV überwacht während der Quantencomputerprogrammlaufzeit den Ablauf des Quantencomputerprogramms während der Ausführung durch die anderen Vorrichtungsteile des Quantencomputers QC. Beim einem Zugriff des Rechnerkerns CPU auf einen bestimmten Adressbereich innerhalb eines Speichers RAM, NVM der Steuervorrichtung µC des Quantencomputers QC oder auf andere vorbestimmte Vorrichtungsteile des Quantencomputers QC erzeugt die Quantencomputerüberwachungsvorrichtung QUV eine Ausnahmebedingung (Exception), insbesondere eine Unterbrechung (Interrupt) des Quantencomputerprogrammablaufs. Woraufhin der Rechnerkern CPU der Steuervorrichtung µC des Quantencomputers QC die Ausführung des Quantencomputerprogramms typischerweise in vorzugsweise vorbestimmter Weise unterbricht.

The document presented here proposes the following to further ensure the functionality of the deployable quantum computer QC with at least one computer core CPU, a control device µC and with a quantum computer monitoring device QUV:

• A quantum computer program should be able to run on the at least one computer core CPU of the control device µC. The quantum computer monitoring device QUV monitors the flow of the quantum computer program during execution by the other device parts of the quantum computer QC during the quantum computer program runtime. When the computer core CPU accesses a specific address area within a memory RAM, NVM of the control device µC of the quantum computer QC or other predetermined device parts of the quantum computer QC, the quantum computer monitoring device QUV generates an exception, in particular an interruption of the quantum computer program flow. Whereupon the computer core CPU of the control device μC of the quantum computer QC typically interrupts the execution of the quantum computer program in a preferably predetermined manner.

The computer core CPU of the control device µC or a central control unit ZSE or another computer system, which can be connected, for example, to the computer core CPU of the control device µC of the quantum computer QC via the external data bus EXTDB, for example the quantum computer monitoring Configure QUV device. The quantum computer QC and/or the computer core µC preferably has means for running through an exception routine after an exception condition has been triggered during the quantum computer program runtime. The exception routine can itself be a quantum computer program.

Further monitoring procedure

• - Überwachen des korrekten Quantencomputerprogrammablaufs des Quantencomputerprogramms des verlegbaren Quantencomputers QC, insbesondere durch die Quantencomputerüberwachungsvorrichtung QUV oder ein andere Rechnersystem;
• - Durchführen vorbestimmter Quantencomputerberechnungen mit mindestens einer Quantenoperation zur Berechnung vorbestimmter Quantencomputerberechnungsergebnisse in vorbestimmten Zeiträumen vor vorbestimmten Zeitpunkten, insbesondere durch den Quantencomputer QC, und
• - Ansteuern einer Quantencomputerüberwachungsvorrichtung QUV nach diesen vorbestimmten Zeitpunkten und Durchführung eines Rücksetzens (Reset-Funktion) oder Reinitialisierens des Quantencomputers QC auf einen vordefinierten Quantencomputerprogrammrestartzustand oder dergleichen, wenn diese Ansteuerung nicht in vorbestimmter Weise erfolgt durchführt.

The document presented here proposes a method for operating a deployable quantum computer system QUSYS with a deployable quantum computer QC and with a quantum computer monitoring device QUV with the following exemplary steps:

• - Monitoring the correct quantum computer program flow of the quantum computer program of the deployable quantum computer QC, in particular by the quantum computer monitoring device QUV or another computer system;
• - Carrying out predetermined quantum computer calculations with at least one quantum operation for calculating predetermined quantum computer calculation results in predetermined time periods before predetermined times, in particular by the quantum computer QC, and
• - Controlling a quantum computer monitoring device QUV after these predetermined times and carrying out a reset (reset function) or reinitialization of the quantum computer QC to a predefined quantum computer program restart state or the like if this control is not carried out in a predetermined manner.

Data buses

The proposed quantum computer QC preferably comprises a data interface DBIF with which the proposed quantum computer QC can communicate with higher-level computer systems du/or other quantum computers QC2 and exchange data. In particular, the proposed quantum computer QC can communicate with a central control unit ZSE via the data interface DBIF and exchange data. The data interface can be wired and/or wireless.

Via the internal data interface MDBIF and the control data bus SDB, the computer core CPU of the control device µC and/or the quantum computer monitoring device QUV with the deployable quantum computer QC can communicate with the device parts of the quantum computer QC and exchange data and signals

Magnetic system

The deployable quantum computer QC preferably includes a system for compensating for external magnetic fields and the earth's magnetic field. For this purpose, the proposed mobile deployable quantum computer QC preferably has a sensor system for three-dimensional detection of the three-dimensional vector of magnetic flux density B. Preferably, the sensor system for three-dimensional detection of the three-dimensional vector of magnetic flux density B detects this three-dimensional vector of magnetic flux density B in the vicinity of the substrate D. For example, the sensor system for three-dimensional detection of the three-dimensional vector of the magnetic flux density B can include three magnetic field sensors MSx, MSy, MSz for the three spatial directions X, Y, and Z. It is conceivable to use a single sensor system if the alignment of the magnetic field allows it. For example, the quantum computer QC may include a magnetic field sensor MSx for the magnetic flux density B _x in the X-axis direction. For example, the quantum computer QC may include a magnetic field sensor MSy for the magnetic flux density B _y in the Y-axis direction. For example, the quantum computer QC may include a magnetic field sensor MSz for the magnetic flux density B _z in the Z-axis direction.

Typically, the proposed mobile quantum computer QC includes magnetic field generating devices PM, MGx, MGy, MGz. The magnetic field generating devices can include permanent magnets PM and/or coils MGx, MGy, MGz, in particular Helmholtz coils and Helmholtz coil pairs, as magnetic field generating means. The permanent magnets PM permanently generate a magnetic flux density. The coils MGx, MGy, MGz generate a magnetic base density according to their electrical current. The permanent magnets PM and the magnetic field generating means MGx, MGy, MGz are preferably part of a magnetic circuit. Preferably, but not necessarily, the magnetic circuit includes a yoke. The permanent magnet PM is preferably located in an air gap. Preferably, a positioning device PV can reposition the permanent magnet PM relative to the substrate D and/or in the air gap and thus change the magnetic flux density B acting on the substrate D with the quantum dots.

The control device µC of the quantum computer QC preferably comprises a navigation device GPS, which informs the computer core CPU of the control device µC of the current position. Preferred The control device µC can use geomagnetic maps of the earth's magnetic field to determine the resulting earth's magnetic field strength and its magnetic flux density component. If the quantum computer QC is moved or rotated translationally, then, for example, the computer core CPU of the quantum computer QC can receive prediction values for future translational coordinates and/or future rotations via the external data bus EXTDB or can predict them from received or determined speed values and rotational speed values. Therefore, the computer core CPU of the quantum computer QC can then make changes to the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in the future Predict magnetic field and compensate by changing the magnetic field generated in the quantum computer QC using the magnetic field generating devices PM, MGx, MGy, MGz.

• In einem ersten Schritt a) stellt die Steuervorrichtung µC bevorzugt beispielsweise mittels Magnetfeldsensoren MSx, MSy, MSz das derzeit wirkende externe Magnetfeld fest. In einem zweiten Schritt erfasst die Steuervorrichtung µC beispielsweise mittels eines Navigationssystems NAV und/oder einer Positionsermittlungsvorrichtung GPS die aktuellen Koordinaten und/oder die aktuelle Geschwindigkeit und/oder Beschleunigung. Auf Basis dieser Daten und ggf. zusätzlicher Daten, wie zum Beispiel einer elektronischen Karte des Erdmagnetfeldes berechnet beispielsweise die Steuervorrichtung µC des verlegbaren Quantencomputers QC das zu erwartende neue externe Magnetfeld und passt bevorzugt die Bestromung der Magnetfelderzeugungsmittel MGx, MGy, MGz so an, dass diese Änderung des externen Magnetfelds durch die Bewegung des Verlegbaren Quantencomputers QC im Wesentlichen nicht wirksam wird und die Berechnungsergebnisse von Quantencomputerprogrammen des verlegbaren Quantencomputers QC im Wesentlichen nicht beeinflussen.

The method for preventing disruptions to the operation of the deployable quantum computer QC due to changes in external magnetic fields as a result of a movement of the deployable quantum computer QC preferably proceeds as follows:

• In a first step a), the control device μC preferably determines the external magnetic field currently in effect, for example using magnetic field sensors MSx, MSy, MSz. In a second step, the control device μC detects the current coordinates and/or the current speed and/or acceleration, for example by means of a navigation system NAV and/or a position determination device GPS. On the basis of this data and possibly additional data, such as an electronic map of the earth's magnetic field, the control device µC of the deployable quantum computer QC, for example, calculates the new external magnetic field to be expected and preferably adjusts the current supply to the magnetic field generating means MGx, MGy, MGz so that they Change in the external magnetic field due to the movement of the deployable quantum computer QC essentially does not take effect and essentially does not affect the calculation results of quantum computer programs of the deployable quantum computer QC.

To simplify the illustration, we assume here that the navigation device GPS not only determines the translational coordinates, for example the position on the earth's surface, but also the angular orientation of the deployable quantum computer QC and the angular velocity of the change in these angles. Only by taking into account the translational changes and the rotational changes in the position and orientation of the deployable quantum computer QC can the computer system CPU of the deployable quantum computer QC suitably predict the necessary adjustment of the magnetic field generation and suitably control the magnetic field generating devices PM, MGx, MGy, MGz.

For this purpose, the computer core CPU of the control device µC can, for example, cause the first magnetic field controller MFSx to adapt the energization of the first magnetic field generating means MGx, which preferably generates a magnetic flux density B _x , with electrical current.

For this purpose, the computer core CPU of the control device µC can, for example, also cause the second magnetic field controller MFSy to adapt the energization of the second magnetic field generating means MGy, which preferably generates a magnetic flux density B _y , with electrical current. For this purpose, the computer core CPU of the control device µC can, for example, also cause the third magnetic field controller MFSz to adapt the energization of the third magnetic field generating means MGz, which preferably generates a magnetic flux density B _z , with electrical current.

For this purpose, the computer core CPU of the control device µC can, for example, also cause the positioning device PV of the permanent magnet PM to spatially adapt the positioning of the permanent magnet PM, which preferably generates a permanent, spatially inhomogeneous magnetic flux density B, and thus the magnetic flux density at the location of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

The computer core CPU of the control device µC preferably detects the actual magnetic field using the said magnetic field sensors MSx, MSy, MSz and regulates the magnetic flux density using the actuators described immediately above in the form of the magnetic field generating devices PM, MGx, MGy, MGz in order to avoid deviations between the detected Vector of the magnetic flux density and the desired vector of the magnetic flux density.

The quantum computer QC preferably comprises an acceleration sensor system that can detect translational and/or rotational accelerations and supplies the corresponding values to the computer core CPU of the control device µC of the quantum computer QC, so that it may take countermeasures in the form of counter-accelerations of a position control system not shown in the figures can. If necessary, the computer core CPU of the control device µC of the quantum computer QC for some such countermeasures use the positioning device PV of the permanent magnet PM and / or the translational positioning device XT in the X direction and / or the translational positioning device YT in the Y direction. The computer core CPU of the control device µC of the deployable quantum computer QC can also, if necessary, modify the focus of the optical system OS depending on such coordinate forecasts and/or speed forecasts and/or acceleration forecasts for translational movements and rotational movements in order to maintain the focus. For example, the computer core CPU of the control device µC of the deployable quantum computer QC can predict deformations and mechanical vibrations within the deployable quantum computer QC based on such coordinate forecasts and/or speed forecasts and/or acceleration forecasts for translational movements and rotational movements and, if necessary, detect these using suitable sensors such as cameras and Detect and compensate for position and distance sensors within the QC quantum computer.

power supply

The deployable quantum computer QC preferably receives its energy from an EV energy supply. A charging device LDV of the energy supply EV receives the energy externally from an energy source PWR.

The book provides a good overview of possible electrical energy sources: Vasily Y. Ushakov (author), “Electrical Power Engineering: Current State, Problems and Perspectives (Green Energy and Technology)”, paperback - August 18, 2018, Springer; 1st ed. 2018 Edition (August 18, 2018), ISBN-10: 3319872850, ISBN-13: 978-3319872858.

• Elektrischer Generator

This energy source can be, for example, one of the following energy sources:

• Electric generator

The energy source can be an electrical generator that converts mechanical energy into electrical energy. The mechanical energy can be, for example, energy transmitted via a wave or the energy of a moving fluid. It can be, for example, an electrical machine, such as a synchronous or asynchronous or direct current motor, a linear motor, a reluctance motor or a BLDC motor or the like, which transfers the mechanical energy of a linear and/or rotational movement by means of induction into lines of a stator and/or or rotor into electrical energy. It can also be a magnetohydrodynamic generator, referred to as an MHD generator for short, which converts the movement of an electrically conductive fluid into electrical energy. The fluid can be a plasma or an electrically conductive liquid, for example a salt solution or a molten metal. The actual energy source can be, for example, a nuclear reactor, an internal combustion engine, a heater, a jet engine, a rocket engine, a ship engine, a Stirling engine, a turbine, a water turbine, a gas turbine, a wind turbine, a tidal power plant, a wave power plant and the like . Magnetohydrodynamic generators, for example, are from the scriptures DE 20 2021 101 169 U1 , WO 2021 159 117 A1 , EP 3 863 165 A1 , US 2021 147 061 A1 , CN 108 831 576 B , US 2019 368 464 A1 , WO 2019 143 396 A2 , EP 3 646 452 B1 , CN 20 634 1126 U , EP 3 279 603 B1 , EP 3 400 642 B1 , EP 3 345 290 B1 , EP 3 093 966 B1 , WO 2016 100 008 A2 , DE 10 2014 225 346 A1 , RU 2014 143 858 A , EP 3 007 350 B1 , US 2016 377 029 A1 , RU 2 566 620 C2 , EP 3 075 064 A1 , EP 2 874 292 B1 , EP 2 986 852 B1 , CN 10 385 5907 B , RU 126 229 U1 , WO 2014 031 037 A2 known. Due to the large number of fonts, the font presented here does not provide a complete list. The document presented here refers to the book Hugo K. Messerle (author), “Magnetohydrodynamic Electrical Power Generation (UNESCO Energy Engineering Series)”, John Wiley & Sons Ltd (August 1, 1995), ISBN-10: 0471942529, ISBN-13 : 978-0471942528.

Electrochemical cell

The energy source can be an electrochemical cell. This can, for example, be an electrochemical cell in the broadest sense, which provides electrical energy through chemical reactions. The document presented includes accumulators, batteries and fuel cells among these electrochemical cells.

Nuclear energy sources

When it comes to nuclear energy sources, the document presented here distinguishes between those that, on the one hand, first convert nuclear energy into mechanical energy, for example using steam cycles and turbines, and then convert it into electrical energy using the generators mentioned above, and on the other hand, nuclear energy convert directly into electrical energy. The document presented here gives examples of betavoltaic cells and thermonuclear generators. These have the advantage that they can be carried out mobile. Therefore they fit particularly good for the technical teaching presented here. The radionuclide batteries considered here preferably use the isotopes ⁶⁰ Co, ⁹⁰ Sr, ¹⁰⁶ Ru, ¹⁴⁴ Cs, ¹⁴⁷ Pm, ²¹⁰ Pm, ²¹⁰ Po, ²³⁸ Pu, ²⁴² Cm, ²⁴¹ Am, ²⁴³ Am. The deployable quantum computer QC is preferably protected from radiation from such a nuclear energy source by radiation shielding, for example made of lead. Radionuclide batteries also include betavoltaic cells, which, for example, convert beta radiation from beta emitters directly into electrical energy.

Such radionuclide batteries are, for example, from the scriptures DE 1 240 967 B , DE 1 564 070 B1 , DE 2 124 465 B2 , DE 7 219 216 U , DE 19 782 844 538 B1 , DE 69 411 078 T2 , US 5,443,657 A , US 5,859,484 A , DE 19 602 875 A1 , DE 19 738 066 A1 , DE 19 957 669 A1 , DE 19 957 669 A1 , US 8,552,616 B2 , WO 2009 103 974 A1 and US 2018 226 165 A1 known.

The energy source can also be a renewable energy source such as a solar cell or a hydroelectric power plant with a water turbine and a generator or a wind turbine with a wind turbine and a generator.

The energy source can also be conventional coal, lignite, oil and gas power plants that burn carbonaceous and/or hydrocarbonaceous fuels to generate thermal energy and then convert the thermal energy into mechanical energy and then convert the mechanical energy into electrical energy.

The energy source can be so-called energy harvesting devices. These are devices that use energy differences that already exist in the environment or otherwise, for example to obtain energy from the kinetic energy of a person or another moving object or from thermal differences, for example in heating systems or the same energy.

Finally, the energy source can simply be the power grid, although the primary energy source can then remain undetermined.

The charging device LDV preferably prepares the energy of the energy supply PWR of the charging device LDV to such an extent that the charging device LDV can charge an energy reserve BENG, BENG2 with the energy of the energy supply PWR. For example, it can be a voltage converter and/or a buck converter or a boost converter or a buck-boost converter depending on the type of power supply PWR. The charging device LDV preferably monitors the charging process of the respective energy reserve BENG, BENG2 when it charges them.

If the quantum computer QC does not execute a quantum computer program and/or does not perform any quantum operations, the charging device LDV can also supply device parts of the deployable quantum computer QC via respective energy processing devices SRG, SRG2. The charging device LDV then preferably also charges one or more of the energy reserves BENG, BENG2 of the deployable quantum computer QC. In the example of the 1 For example, the proposed deployable quantum computer QC has two energy reserves BENG, BENG2 and two energy processing devices SRG, SRG2. The document presented here indicates that the number of energy reserves, energy processing devices and charging devices and separation devices is greater than in the example of 2 can be.

Although the charging device LDV represents a barrier to transients in the power supply PWR, the charging device LDV cannot generally completely suppress these transient disturbances in the power supply PWR. The charging device LDV also produces transient disturbances itself, for example if the charging device LDV is a switching power supply. It has therefore proven useful to have one or more low-noise energy reserves BENG, BENG2 for supplying device parts that are particularly susceptible to interference, such as the photodetector PD, the amplifier V, the light source driver LDRV, the light source LD and, if necessary, for device parts MFSx, MFSy, MFSz, MGx that generate magnetic fields. MGy, MGz and device parts with a particularly time-sensitive signal scheme such as the waveform generator WFG and the microwave and / or radio wave frequency generator MW / RF-AWFG to generate largely freely definable waveforms (English: arbitrary wave form generator). Particularly preferably, these device parts stabilize their internal supply voltages again within these device parts in order to maximally suppress the noise and disturbances in the energy supply. The quantum computer QC preferably comprises one or more energy processing devices SRG, SRG2 for supplying the device parts from the one energy reserve or the plurality of energy reserves BENG, BENG2. The energy processing devices preferably adapt the voltage level that is supplied by the charging device LDV or the energy reserves BENG, BENG2 to the required voltage levels of the device part of the quantum computer QC that is supplied, preferably with a voltage reserve. In one second control stage, which is preferably a linear regulator, these linear regulators can then, for example, use the voltage reserve to adjust the actual supply voltage of the relevant device parts of the quantum computer QC with low noise and precisely.

One or more separating devices TS preferably separate the one charging device or the several charging devices LDV from the one energy processing device or the several energy processing devices SRG, SRG2 and / or the one low-noise energy reserve or from the several low-noise energy reserves BENG, BENG2, if the quantum computer is a Executes quantum computer program and/or performs a quantum operation. A quantum operation in the sense of the document presented here is a manipulation of a quantum dot NV1, NV2, NV3 and/or a core quantum dot CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . In the sense of the document presented here, a quantum computer program is a program that includes at least one quantum operation. One or more binary data in the memory NVN, RAM of the control device μC of the deployable quantum computer QC preferably encode such a quantum operation. For example, it can be a predetermined data word. A quantum operation in the sense of the document presented here manipulates at least the quantum state of at least one quantum dot of the quantum dots NV1, NV2, NV3 of the deployable quantum computer QC and/or manipulates at least the quantum state of at least one core quantum dot of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the deployable quantum computer QC. The technical teaching of the document presented here also refers to the data word that symbolizes such a quantum operation as a quantum op code. A quantum computer program includes at least one quantum op-code. In the above case, when the deployable quantum computer QC executes a quantum computer program and/or carries out a quantum operation, the one or more energy reserves BENG, BENG2 preferably supply the one or more energy processing devices SRG, SRG2 with electrical energy, which is particularly is low noise.

One or more separating devices TS preferably connect the one charging device or the several charging devices LDV with the one energy processing device or the several energy processing devices SRG, SRG2 and / or the one low-noise energy reserve or one of the several low-noise energy reserves BENG, BENG2, if the deployable quantum computer QC does not execute a quantum computer program and/or does not perform a quantum operation. In this case, the charging device LDV preferably charges the one energy reserve or the several energy reserves BENG, BENG2 and, if necessary, supplies the one energy processing device or the several energy processing devices SRG, SRG2 with electrical energy, which typically now has less noise.

Magnetic field shielding

In order to reduce the influence of external magnetic fields, it makes sense if the proposed quantum computer QC is provided with a shield AS for these external magnetic fields. This shielding can be, for example, a passive shielding AS, for example in the form of µ-metal mats, and/or an active shielding AS in the form of a magnetic field-generating system, which generates a magnetic counterfield to an external magnetic interference field and thereby reduces its effect and/or or even compensated. The proposed quantum computer therefore preferably comprises one or more sensors MSx, MSy, MSz for detecting the strength of the magnetic flux density B and/or the magnetic field strength H. The control device preferably uses the μC detected by the one or more sensors MSx, MSy, MSz Values of the magnetic flux density B and/or the magnetic field strength H for controlling magnetic field generating means MGx, MGy, MGz. The magnetic field generating means MGx, MGy, MGz preferably generate a compensating magnetic flux density B of a magnetic counterfield that compensates for the magnetic flux density B of the magnetic interference field.

A first sensor MSx preferably detects the strength of the magnetic flux density B and/or the magnetic field strength H in a first direction, for example an X-axis. A first magnetic field control MFSx preferably supplies a first magnetic field generating means MGx with electrical energy. The first magnetic field generating means MGx preferably generates a magnetic flux density B _x , which preferably essentially has a direction that preferably corresponds to the first direction, for example the direction of the X-axis. The first magnetic field control MFSx preferably supplies the first magnetic field generating means MGx with a first electrical current Ix. The control device µC preferably controls the first magnetic field generating means MGx via the first magnetic field control MFSx. The first magnetic field control MFSx preferably regulates the generation of the magnetic flux density B _x by the first magnetic field generating means MGx in such a way that the magnetic flux density B detected by the first sensor MSx or that by the first sensor MSx detected magnetic field strength H corresponds to a first value. This first value is preferably zero. For this purpose, the first magnetic field controller MFSx evaluates the value of the magnetic flux density B detected by the first sensor MSx or the value of the magnetic field strength H detected by the first sensor MSx.

A second sensor MSy preferably detects the strength of the magnetic flux density B and/or the magnetic field strength H in a second direction, for example a Y-axis. The direction of the Y-axis is preferably chosen perpendicular to the direction of the X-axis. A second magnetic field control MFSy preferably supplies a second magnetic field generating means MGy with electrical energy. The second magnetic field generating means MGy preferably generates a magnetic flux density B _y , which preferably essentially has a direction that preferably corresponds to the second direction, for example the direction of the Y axis. The second magnetic field control MFSy preferably energizes the second magnetic field generating means MGy with a second electrical current Iy. The control device µC preferably controls the second magnetic field generating means MGy via the second magnetic field control MFSy. The second magnetic field control MFSy preferably regulates the generation of the magnetic flux density B _y by the second magnetic field generating means MGy in such a way that the magnetic flux density B detected by the second sensor MSy or the magnetic field strength H detected by the second sensor MSy corresponds to a second value. This second value is preferably zero. For this purpose, the second magnetic field control MFSy evaluates the value of the magnetic flux density B detected by the second sensor MSy or the value of the magnetic field strength H detected by the second sensor MSy.

A third sensor MSz preferably detects the strength of the magnetic flux density B and/or the magnetic field strength H in a third direction, for example a Z-axis. The direction of the Z-axis is preferably selected perpendicular to the direction of the X-axis and perpendicular to the direction of the Y-axis. A third magnetic field control MFSz preferably supplies a third magnetic field generating means MGz with electrical energy. The third magnetic field generating means MGz preferably generates a magnetic flux density B _z , which preferably essentially has a direction that preferably corresponds to the third direction, for example the direction of the Z-axis. The third magnetic field control MFSz preferably supplies the third magnetic field generating means MGz with a third electrical current Iz. The control device µC preferably controls the third magnetic field generating means MGz via the third magnetic field control MFSz. The third magnetic field control MFSz preferably regulates the generation of the magnetic flux density B _z by the third magnetic field generating means MGz in such a way that the magnetic flux density B detected by the third sensor MSz or the magnetic field strength H detected by the third sensor MSz corresponds to a third value. This third value is preferably zero. For this purpose, the third magnetic field controller MFSz evaluates the value of the magnetic flux density B detected by the third sensor MSz or the value of the magnetic field strength H detected by the third sensor MSz.

The proposed deployable quantum computer QC typically has an optical system OS that allows the light source LED to irradiate the quantum dots NV1, NV2, NV3 with pump radiation LB. The optical system OS is preferably a confocal microscope. The optical system OS preferably also enables the optical reading of the state of quantum dots NV1, NV2, NV3 of the deployable quantum computer QC. For this purpose, the deployable quantum computer QC of the deployable quantum computer system QUSYS, for example, preferably has a dichroic mirror DBS, which allows the fluorescent radiation FL emitted by the quantum dots NV1, NV2, NV3 to pass and directs the pump radiation LB of the light source LD onto the quantum dots NV1, NV2, NV3 and keeps the pump radiation LB from the photodetector PD for detecting the fluorescence radiation FL. Instead of a dichroic mirror DBS, the deployable quantum computer QC of the quantum computer system QUSYS can, for example, also have a dichroic mirror DBS, which reflects away the fluorescent radiation FL emitted by the quantum dots NV1, NV2, NV3 and the pump radiation LB of the light source LD via the optical system OS onto the quantum dots NV1, NV2, NV3 passes through, so that the pump radiation LB of the light source LD irradiates these quantum dots NV1, NV2, NV3 with pump radiation LB of the pump radiation wavelength λ _pmp . In this case, the optical system OS preferably detects the fluorescence radiation FL of the quantum dots NV1, NV2, NV3 and the dichroic mirror DBS reflects this fluorescence radiation FL onto the photodetector PD for detecting the fluorescence radiation FL. The proposed deployable quantum computer QC therefore comprises, if it uses an optical readout of the states of the quantum dots NV1, NV2, NV3, a photodetector PD for detecting the fluorescence radiation FL of the quantum dots NV1, NV2, NV3. The photodetector PD typically generates a received signal S0 depending on the fluorescence radiation FL. An amplifier V following in the signal path typically amplifies and filters the received signal S0 to an amplified received signal S1. The amplifier V is therefore typically used for amplification and/or Filtering the output signal of the photodetector PD, which is typically the received signal S0. The amplified received signal S1 is preferably a digitized signal consisting of one or more sample values. The control device μC preferably detects the value of the amplified received signal S1, for example by means of an analog-to-digital converter ADCV. The deployable quantum computer QC according to the proposal includes, if it uses an electronic readout of the states of the quantum dots NV1, NV2, NV3, a corresponding device for electronically reading out the states of the quantum dots NV1, NV2, NV3. At this point the document presented here expressly refers to the document again DE 10 2020 125 189 A1 . These device parts are preferably accommodated in a preferably common housing GH, which is preferably part of the deployable quantum computer QC in the sense of the document presented here. As already described above, the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₂ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are preferably located within said substrate D. The substrate D is preferably doped with dopants. Preferably, the substrate D essentially comprises essentially atoms without a magnetic moment, at least in the effective area of the quantum dots NV1, NV2, NV3. In the case of diamond as the material of the substrate D, the diamond preferably comprises essentially ¹² C isotopes. In the case of using NV centers in diamond as quantum dots, NV1, NV2, NV3 particularly preferably form oxygen atoms ¹⁶ O, ¹⁸ O and/or phosphorus and/or sulfur atoms ³² S, ³⁴ S, ³⁶ S without a magnetic moment in the substrate D the doping in the area of the quantum dots NV1, NV2, NV3. This doping in the area of the quantum dots NV1, NV2, NV3 has two tasks. First, these doping atoms change the Fermi level E _F in the region of the quantum dots NV1, NV2, NV3. In the case of using NV centers as quantum dots NV1, NV2, NV3, this doping with said doping atoms shifts the Fermi level E _F in the area of these quantum dots NV1, NV2, NV3. In the case of n-doping, this n-doping shifts the Fermi level E _F in the area of these quantum dots NV1, NV2, NV3 in such a way that the Fermi level is raised and that the NV centers that are lower in energy are then preferably negatively charged are. The NV centers then represent NV centers. Since NV centers have a magnetic moment of this electron configuration due to the negative charge electron, ^NV centers are therefore particularly suitable for use as quantum dots NV1, NV2, NV3. Secondly, this doping, which is preferably an n-doping, means that the vacancies in the diamond are electrically charged during the implantation to form the NV centers and therefore do not aggregate due to the electrical repulsion of the negatively charged individual defects . As a result, the concentration of individual defects remains high, which increases the likelihood of NV centers forming when nitrogen is implanted in diamond. The best results are achieved by doping a diamond substrate D with sulfur before nitrogen implantation. Doping with a sulfur isotope without a nuclear magnetic moment is preferred. Such isotopes are the isotopes ³² S, ³⁴ S, ³⁶ S. An alternative is doping with the oxygen isotopes ¹⁶ O, ¹⁸ O, but this is less suitable. It is known that n-doping with phosphorus is also said to be successful. However, phosphorus has a nuclear magnetic moment. In principle, N-doping with atoms that have no magnetic nuclear moment makes sense. A shift in the Fermi level E _F by other means, for example by means of preferably very thin electrodes precharged to a suitable potential relative to the substrate D, also led to such effects in advance of the preparation of this document. The substrate D of the deployable quantum computer therefore preferably has a local shift in the Fermi level E _F at least temporarily, so that it is then energetically shifted in such a way that the yield of quantum dots NV1, NV2, NV3 in the form of NV centers during the implantation of the Nitrogen atoms is increased. In an analogous manner, the Fermi level E _F of other substrate materials and/or in relation to other paramagnetic centers (eg the ST1 center) can be influenced in the formation of these paramagnetic centers. Preferably there are the light source LD and the light source driver LDRV and the substrate D and the devices for generating the electromagnetic wave field MW/RF-AWFG, mWA, MGx, MGy, MGz and the control device µC and the memories RAM, NVM of the control device µC and that optical system OS and possibly the amplifier V and the shield AS are located within the housing GH, whereby they are preferably shielded from electromagnetic interference radiation penetrating from outside. For this purpose, the material of the housing GH preferably comprises an electrically conductive material. The housing GH preferably forms a Faraday cage. The material of the housing GH preferably also includes a material for shielding magnetostatic and/or quasi-static magnetic fields. For this purpose, the material of the housing GH preferably comprises so-called µ-metal, which is a particularly soft magnetic material.

The preferred p-metal proposed here for use in quantum computers QC and quantum technology devices (Mumetall, English: “mu-metal” or English: “permalloy”) typically belongs to a group of soft magnetic nickel-iron alloys with 72 to 80% nickel and proportions of copper, molybdenum, cobalt or chromium with high magnetic permeability is used in the proposed deployable quantum computer QC or the proposed quantum technological device for shielding AS from low-frequency external magnetic fields.

According to the proposal, such µ-metal has a high permeability (µ _r =50,000 to 140,000 or more), which causes the magnetic flux of the external low-frequency magnetic fields to concentrate in the material of the housing GH of the deployable quantum computer QC. This effect leads to considerable shielding attenuation when shielding AS from low-frequency or static magnetic interference fields. Thus, the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are shielded against such external magnetic fields even when the deployable quantum computer QC changes the spatial orientation and/or location in the course of a relocation, with such a change in the orientation of the relocatable quantum computer QC and/or the change in location of such a relocatable quantum computer QC typically resulting in a change in the orientation and/or the strength of the magnetic fields act on the deployable quantum computer QC, relative to the deployable quantum computer QC. This is particularly advantageous if the deployable quantum computer QC, for example to save weight, does not have active shielding against external magnetic fields, which would detect the interfering magnetic field using a magnetic field sensor MSX, MSy, MSz and using suitable means MFSx, MFSy, MFSz, MGX, MGy, MGz would generate a magnetic opposing field for compensation.

The document presented here also suggests, among other things, that the shield AS of the quantum computer QC can be part of the housing GH of the deployable quantum computer QC or the housing GH of the deployable quantum computer QC itself. As already described, the control device µC controls the light source LD with the aid of said light source driver LDRV. The control device μC preferably generates a light source control signal, which can be the transmission signal S5, for example, by means of suitable means. The light source driver LDRV then typically supplies the light source LD with electrical energy depending on the light source control signal from the control device μC. The light source LD thus preferably generates the pump radiation LB depending on the light source control signal from the control device μC. Preferably, the light source LD therefore generates the pump radiation LB, preferably depending on the transmission signal S5. In that case the 1 The control device μC transmits the light source control signal preferably via the control data bus SDB and the waveform generator WFG as a transmission signal S5. In the following, the reader can therefore assume, for the sake of simplicity and better understanding, that in the 1 the light source control signal is equal to the transmission signal S5. The light source LD then irradiates the quantum dot or the multiple quantum dots NV1, NV2, NV3 by means of the optical system OS with pump radiation LB of a pump radiation wavelength λ _pmp. The pump radiation wavelength λ _pmp is preferably between 400 nm and 700 nm wavelength and/or better between 450 nm to 650 nm and/or better between 500 nm to 550 nm and/or better between 515 nm to 540 nm and/or optimally at a wavelength of 532 nm. In the case of NV centers in diamond, a laser diode from the company. Osram type PLT5 520B with 520nm wavelength has proven itself as an exemplary source of pump radiation LB for the irradiation of NV centers in diamond as the material of substrate D. The quantum dots NV1, NV2, NV3 then emit fluorescence radiation FL with a fluorescence wavelength λ _fl depending on their state and on the pump radiation LB. In the case of NV centers as paramagnetic centers of quantum dots, the <fluorescence wavelength is typically in the range of 638 nm. The intensity l _fl of the fluorescence radiation FL typically depends on the intensity l _pmp of the pump radiation LB and thus also on the light source control signal. The one quantum dot or the multiple quantum dots NV1, NV2, NV3 thus emit fluorescence radiation FL with a fluorescence radiation wavelength λ _fl when irradiated with electromagnetic radiation of the pump radiation wavelength λ _pmp . In the case of an optical readout of the state of the quantum dots NV1, NV2, NV3 or the quantum dot, the photodetector PD detects the fluorescence radiation FL by means of the optical system OS and converts the fluorescence radiation FL into a receiver output signal S0. The receiver output signal S0 typically depends on the fluorescent radiation FL striking the photodetector PD. The receiver output signal S0 preferably depends on the intensity l _fi of the fluorescent radiation FL that hits the photodetector PD. In the case of optical reading of the state of the quantum dot(s) NV1, NV2, NV3, the amplifier V amplifies and/or filters the receiver output signal S0 and preferably makes the signal available to the computer core CPU of the control device µC as an amplified received signal S1. The amplifier V preferably sets the values of the samples of the amplified sample values of the amplified emp, which are digitized by means of an analog-to-digital converter of the amplifier V interception signal S1 in a memory of the amplifier V. The computer core CPU of the control device µC of the deployable quantum computer QC can then query and further process these sample values of the amplified received signal S1 from the memory of the amplifier V, for example via the control data bus SDB. In the case of electronic reading of the quantum dots NV1, V2, NV3 generate in 1 For a better overview, devices HS1 to HS3 and VS1, not shown, for electronically reading out the states of the quantum dots NV1, NV2, NV3 with a control unit B CBB a second received signal. As already described, the control device µC of the deployable quantum computer QC controls the one or more devices for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . By controlling one or more devices (LH1, LH2, LH3, LV1) for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or by controlling the emission of the light source LD, the control device μC of the deployable quantum computer QC can thus control the states of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ change and/or link with each other. The control device μC of the deployable quantum computer QC preferably has means for generating a measured value signal with one or more measured values from one or more received signals, in particular from the first received signal and/or the second received signal. Since these received signals depend on the states of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ , the measured value signal typically also depends of states of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

To achieve deployability, the use of a room temperature deployable QC quantum computer based on paramagnetic centers as quantum dots NV1, NV2, NV3 using nuclear magnetic moments as core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ has been used so far , CI3 ₁ , CI3 ₂ , CI3 ₃ with optical pump radiation LB and optical state readout or electronic state readout of the quantum dot states of the quantum dots NV1, NV2, NV3 and a suitable deployable, preferably passive shielding AS proposed.

The proposal presented here now suggests that the deployable quantum computer QC and/or the mobile device has a deployable energy supply EV for supplying the deployable quantum computer QC with energy. This is the only way to complete the installability. The energy supply EV is preferably located within the housing GH. The housing GH can comprise a partial housing with a magnetically shielded area in which the partial devices of the deployable quantum computer QC that are sensitive to magnetic fields are located. Outside this partial housing, but still within the housing GH, there are preferably the parts of the deployable quantum computer QC which, firstly, are not or less sensitive to external magnetic and electromagnetic interference fields and/or themselves generate electromagnetic and/or magnetic interference fields. The energy supply EV is therefore preferably placed outside the partial housing within the housing GH of the deployable quantum computer QC. The quantum computers QC1 to QC16 of a quantum computer system QUSYS can also have a common housing GH.

Typically, the proposed deployable quantum computer QC, together with all the means necessary for its operation, is part of the deployable quantum computer system QUSYS, for example the smartphone or the portable quantum computer system QUSYS or the vehicle or the deployable weapon system.

These means for operating the deployable quantum computer QC must therefore also be deployable. The proposed deployable quantum computer system QUSYS includes deployable means for its operation and in particular one or more deployable energy supplies EV and/or one or more deployable quantum computers QC. For the purposes of this document, these means for operating the deployable quantum computer QC are also part of the smartphone or the item of clothing or the portable quantum computer system QUSYS or the vehicle or the deployable weapon system. It is irrelevant to the interpretation of the claims whether the operation of the deployable quantum computer QC is coupled to means and/or commands outside the quantum computer QC despite the presence of all means for operating the deployable quantum computer QC as part of the deployable quantum computer QC. It is important that the deployable quantum computer QC is potentially functional without these resources and/or commands outside the quantum computer QC. For example, a deployable quantum computer system QUSYS should be based on the programming of the central control device ZSE and/or the programming of a Control device µC of a quantum computer QC of the quantum computer system QUSYS waits for an external start command, still be covered by the claims.

The mobile, deployable energy supply EV preferably comprises one or more deployable charging devices LDV with one or more energy supplies PWR of the charging device en LDV, one or more deployable separation devices TS, one or more deployable energy reserves BENG and one or more deployable energy processing devices SRG. The mobile energy supply EV preferably comprises an energy processing device SRG, in particular a voltage converter or a voltage regulator or a current regulator, which prevents changes in the energy content of the energy reserve BENG of the energy supply EV, for example the state of charge of a battery as an energy reserve BENG of the energy supply EV, from affecting the relocatable quantum computer QC and/or the quantum computer system QUSYS. The mobile energy supply EV supplies the energy processing device SRG with energy and the energy processing device SRG, for example, supplies the deployable quantum computer QC and possibly other parts of the quantum computer system QUSYS with electrical energy. In this case, the energy supply EV, for example, only supplies the quantum computer QC with electrical energy indirectly via the energy processing device SRG.

Typically, according to the proposal, the deployable quantum computer QC is set up and intended to be able to work with a reduced first number of quantum dots NV1, NV2, NV3 even at room temperature. Room temperature as the operating temperature of the quantum dots NV1, NV2, NV3 leads to a broadening of the resonances in the resonance spectrum, so that they overlap. The proposed deployable quantum computer QC therefore preferably has a deployable cooling device KV, which can be deployed together with the deployable quantum computer QC. The relevant relocatable cooling device KV is preferably suitable and/or intended to control the temperature of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1, CI2 ₂ , _{CI2 3 ,} CI3 ₁ , CI3 ₂ , CI3 ₃ to lower. Lowering the operating temperature of the quantum dots NV1, NV2, NV3 leads to a narrowing of the resonances in the resonance spectrum, so that they overlap to a lesser extent or not at all. Such cooling by means of a cooling device KV preferably lowers the temperature of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ to this extent that the quantum computer QC can work with a second number of quantum dots NV1, NV2, NV3 that is increased compared to the first number of quantum dots NV1, NV2, NV3.

The deployable quantum computer QC preferably comprises, as the deployable cooling device KV, a closed loop helium gas cooling system HeCLCS, also referred to as a closed cycle cryocooler. For example, we refer to https://en.wikipedia.org/wiki/Cryocooler.

A further embodiment of the proposal concerns a deployable quantum computer that has a deployable second deployable power supply. The relocatable second power supply can be completely or partially identical to the first relocatable power supply (BAT). This second relocatable energy supply BENG preferably supplies the relocatable cooling device KV with energy. This has the advantage that the first energy supply is not disturbed by transient disturbances in the electric motors of the relocatable cooling device KV.

Another embodiment of the proposal concerns a deployable quantum computer QC for use in a mobile device. Use in a smartphone or a portable quantum computer system QUSYS or in a vehicle or in a weapon system is particularly preferred. This means that the document presented here proposes a deployable weapon system with a deployable quantum computer QC, which is part of the deployable weapon system. The use of the deployable quantum computer QC as part of the fire control system of the weapon system or the navigation system GPS, NAV of the weapon system is particularly preferred. The weapon system particularly preferably uses the deployable quantum computer QC to solve NP-complete problems, such as, but not only, the identification of targets, the classification of targets, the assignment of targets to known enemy objects such as aircraft and/or missile types, vehicle types, ship types, Types of missiles, types of floating bodies, types of underwater vehicles, types of underwater objects, types of spacecraft, types of satellites, etc. Furthermore, the selection of the order of attacking the targets and/or the selection of weapons and/or the selection of ammunition for combating the targets can be included Problems that the weapon system solves with the help of the deployable quantum computer QC. In addition, the deployable weapon system can use the deployable quantum computer QC to determine and/or modify and/or monitor the route of the respective projectile or warhead or weapon carrier to the target using the deployable quantum computer QC.

Such a method begins with the acquisition of environmental data by the QUSYS quantum computer system in step A). The environmental data is typically collected using suitable sensors, which can be part of the quantum computer system QUSYS or which are connected to this quantum computer system QUSYS via data connections and transmit environmental data to the quantum computer system QUSYS. In a step B), the quantum computer system QUSYS identifies objects in the environment of the quantum computer system QUSYS, whereby this environment can also be distant from the quantum computer system QUSYS. In step C), the quantum computer system QUSYS classifies the identified objects in the environment of the quantum computer system QUSYS. Typically, in step C), the quantum computer system QUSYS classifies the objects according to danger and/or vulnerability and/or strategic effect in order to maximize a weapon effect. This classification is preferably carried out in step C) using a neural network model, which the quantum computer system QUSYS preferably executes. For this step C), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out the classification of the objects. In a step D, the quantum computer system QUSYS determines the weapons and/or the ammunition and/or the configuration and/or the order of the attacked objects and/or the attacked and/or the non-attacked objects. This determination is preferably carried out in step D) using a neural network model, which the quantum computer system QUSYS preferably executes. In step D), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out these determinations. In a step E), the quantum computer system QUSYS preferably suggests one or more of these specified attack scenarios to an operator, for example one or more pilots and/or several fire control officers or the like. If they give the command to fire, the QUSYS quantum computer system can, for example, implement the released attack scenario in a step F). This is in 12 shown.

The deployable quantum computer QC preferably has a shield AS. The shield AS preferably shields the quantum dots NV1, NV2, NV3, for example the NV centers, against electromagnetic fields and/or electromagnetic waves.

The deployable quantum computer QC preferably comprises an optical system OS that directs the electromagnetic radiation from the light source LD onto the quantum dots NV1, NV2, NV3, for example the paramagnetic centers or the NV centers. The optical system OS preferably includes a confocal microscope.

The optical system OS preferably comprises a first camera CM1, which detects the fluorescence radiation FL of the paramagnetic centers NV1, NV2, NV3 and/or clusters of such paramagnetic centers, for example NV centers and/or clusters of NV centers. Other fluorescent defect centers with other fluorescence wavelengths are conceivable. Such other fluorescent defect centers with other fluorescence wavelengths can thus have fluorescence radiation with a fluorescence wavelength that is different from the fluorescence wavelength λ _fl of the quantum dots NV1, NV2, NV3 and therefore, for example, by means of a dichroic mirror instead of the semi-transparent mirror STM or by means of an optical filter the pump radiation LB and the fluorescence radiation FL of the quantum dots NV1, NV2, NV3 can be optically separated. The substrate D is preferably stored on a positioning table. The positioning table preferably comprises a translational positioning device XT in the X direction and a translational positioning device YT in the Y direction, which preferably controls the control device μC of the quantum computer QC via the control data bus SDB. The first camera CM1 preferably detects the position of the substrate D relative to the optical system OS and thus the position of the quantum dots NV1, NV2, NV3 in the substrate D. The first camera CM1 thus detects the position of the paramagnetic centers, for example the NV centers, relative to the optical system OS. If the substrate D shifts relative to the optical system OS, for example due to mechanical vibrations or other disturbances, an image processing system of the deployable quantum computer QC detects this mechanical displacement, for example by evaluating the position of fluorescent paramagnetic defect centers. The image processing system preferably detects the fluorescence patterns of the defect centers using the first camera CM1 and compares their position on the image with target positions. The image processing system preferably determines a displacement vector and repositions the substrate D using the positioning table XT, YT relative to the optical system OS depending on the determined displacement vector. The image processing device preferably carries out this repositioning in such a way that the position of the Quantum dot, for example the paramagnetic center or a cluster of paramagnetic centers, is preferably substantially unchanged relative to the optical system OS after completion of the repositioning. The image processing system is preferably part of the deployable quantum computer QC. Typically, the controller µC of the quantum computer works as the image processing system. However, the image processing system can also be a separate sub-device of the deployable quantum computer QC. In this case, the control device μC preferably controls the separate image processing system via the control data bus SDB. The image processing system can then be part of the first camera interface CIF, for example. Instead of an image processing system, other position displacement sensors can also detect the displacements of the substrate D relative to the optical system. The proposed quantum computer QC then adjusts the position of the substrate D relative to the optical system OS based on the position displacement data of such position displacement sensors. For example, such position displacement sensors can transmit the detected position displacement data to the control device µC of the quantum computer QC via the control data bus SDB, so that the control device µC of the quantum computer QC, for example depending on this detected position displacement data via the control data bus SDB, moves the positioning table by means of the translational positioning device XT in the X direction and by means of the translational positioning device YT in the Y direction, the control device µC repositions the substrate D relative to the optical system OS depending on this determined position displacement data as if essentially no displacement had taken place. This ensures that the deployable QC quantum computer also works with vibrations, accelerations and the like.

The deployable quantum computer QC preferably comprises a photodetector PD and an amplifier V. The photodetector PD detects the fluorescent radiation FL of the quantum dots NV1, NV2, NV3 when the light source LD irradiates it with its electromagnetic radiation, which serves as pump radiation LB. The deployable quantum computer QC preferably uses this to read out the quantum state of the quantum dots NV1, NV2, NV3. The quantum dots NV1, NV2, NV3 are preferably paramagnetic centers. Quantum dots NV1, NV2, NV3. The paramagnetic centers are preferably NV centers in diamond. The amplifier V amplifies and/or filters the receiver output signal S0 of the photodetector PD to an amplified receiver output signal S1. The amplified receiver output signal can, for example, also be an ordered amount of data in a memory of the amplifier V, the computer core CPU of the control device μC preferably being able to read out this memory of the amplifier V at least partially via the control data bus SDB.

Furthermore, the deployable quantum computer QC can also carry out an electronic readout of quantum dots NV1, NV2, NV3 in parallel or as an alternative to this optical reading of the state of quantum dots NV1, NV2, NV3. For this purpose, the deployable quantum computer QC can have, alternatively or in parallel to the photodetector PD and the amplifier V, a device for electronically reading out the states of the quantum dots NV1, NV2, NV3. The device for electronically reading out the states of the quantum dots NV1, NV2, NV3 preferably comprises electrically conductive lines for applying electric fields in the effective area of the quantum dots NV1, NV2, NV3 and contacts for extracting charge carriers in the area of the quantum dots NV1, NV2, NV3. Furthermore, the device for electronically reading out the states of the quantum dots NV1, NV2, NV3 preferably comprises devices for providing the control signals for controlling said electrically conductive lines for applying electric fields in the effective range of the quantum dots NV1, NV2, NV3. Furthermore, the device for electronically reading out the states of the quantum dots NV1, NV2, NV3 preferably includes devices for amplifying the electrical currents of charge carriers sucked out via the contacts for suctioning off charge carriers in the area of the quantum dots NV1, NV2, NV3. The proposed quantum computer QC preferably has one or more digital-to-analog converters, which are involved in generating the control signals for driving said electrically conductive lines LH1, LH2, LH3, LV1 for applying electric fields in the effective range of the quantum dots NV1, NV2 , NV3 contribute. For controlling the first quantum dot NV1 to be controlled, the first horizontal driver stage HD1 preferably has an analog-to-digital converter, which the computer core CPU of the control device μC can preferably control via the control data bus STB. For controlling the second quantum dot NV2 to be controlled, the second horizontal driver stage HD2 preferably has an analog-to-digital converter, which the computer core CPU of the control device μC can preferably control via the control data bus STB. The third horizontal driver stage HD3 preferably has an analog-to-digital converter for controlling the third quantum dot NV3 to be controlled, which the computer core CPU of the control device µC can be preferably controlled via the control data bus STB. The control device µC preferably controls one or more of these digital-to-analog converters via an internal control data bus SDB of the deployable quantum computer QC.

This hardware (Q-circuit hardware model) of the quantum gate hardware model 11 includes means mWA, LH1, LV1, LV2 for influencing the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ using electromagnetic HF waves and/or electromagnetic microwaves and MW/RF-AWFG means for driving these means. This hardware (Q-circuit hardware model) of the quantum gate hardware model 11 includes means LD, OS for influencing the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ using optical pump radiation LB and means WFG, LDRV for controlling these means. This hardware (Q-circuit hardware model) of the quantum gate hardware model 11 includes means LH1, LV1, LV2 for selecting the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ using static electromagnetic fields and means for controlling these means. This hardware (Q-circuit hardware model) of the quantum gate hardware model 11 thus includes means such as radio wave lines and components, microwave lines and components (RF, HF lines), an optical system, and an electric grid, such as the DE 10 2020 125 169 A1 in your 20 shows. On the 23 the DE 10 2020 125 169 A1 and their associated description is also referred to in the document presented here. The optical system OS is preferably a confocal microscope with a pulsable laser as the light source LD.

A gate pulse timing device, which typically includes the microwave and radio frequency generator MW/RF-AWFG, generates the control signals for timely generation of the signals on the radio wave lines and microwave lines LH1, LV1, LV2. A laser control device (laser control), typically comprising a waveform generator WFG and a light source driver LDRV and the laser as a light source LD, with which the optical system OS is fed with typically pulsed pump radiation LB. An input-output signal generation (I/O) signal controls the selection of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ taking part in a quantum operation , CI3 ₂ , CI3 ₃ the DC voltage and DC level components of the electrical grid s (electrical grid) comprising the control lines LH1, LV1, LV2. A sequential control system (SPC) controls the entire process. The sequence control preferably comprises a control device μC of the quantum computer QC. Preferably, the optical system for reading out the quantum state of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ includes a photodetector PD for detection of electromagnetic radiation from the quantum dots of the quantum dots NV1, NV2, NV3 with amplifier V, filter etc.

The architecture of the hardware (Q-circuit hardware model) of this quantum computer QC therefore preferably corresponds essentially to the architecture of the 23 the DE 10 2020 125 169 A1 .

This quantum computer QC is now preferably equipped with a central control unit (reference number ZSE in 38 the DE 10 2020 125 169 A1 tied together). Without having to mention this elsewhere in this document, the central control unit ZSE of a quantum computer system QUSYS can take over tasks of one or more control devices µC of one or more quantum computers of the quantum computers QC1 to QC16 of a quantum computer system QSYS. To simplify matters, this document describes the division of labor between the one or more control devices μC of one or more quantum computers of the quantum computers QC1 to QC16 of a quantum computer system QSYS on the one hand and the central control device ZSE of a quantum computer system QUSYS in this document always as if the control devices mc primarily take over these tasks , without limiting the possible division of tasks to this. Other divisions of tasks are therefore an express part of the disclosure of the document presented here.

The central control device µC of the quantum computer QC executes a control method (transcompiler) in the form of a control program called a transcompiler 9, which converts control commands (mnemonics) of the quantum technological algorithms 8 into concrete control signals for the hardware components described above, which the control device µC uses over one or more Control data buses SDB transmitted. An optimizer, which is typically part of the transcompiler 9, optimizes, if necessary, setting parameters and possibly filter parameters in the form of an optimization process that the central control unit µC typically carries out and, if necessary, processes measurement signals of the optical system OS, PD, V . The control device µ0 of the quantum computer QC typically carries out a quantum error correction method (QEC), which is typically part of the transcompiler 9, in the form of a quantum error correction program, which the central control unit µC typically carries out. The quantum error correction program corrects the errors that certainly occur due to the statistical behavior of the quantum bits of the quantum dots NV1, NV2, NV3 and the core quantum bits of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ . The control methods that the control device µC typically carries out and which symbolize the control commands (mnemonics) preferably essentially correspond to abstract quantum operations (Abstract Q-circuit models) of abstract quantum gate models 8, which the control device µC typically carries out. The control device µC carries out summaries of such methods as quantum calculations (quantum algorithms, quantum technology algorithms 7). In addition to these quantum-specific components, a proposed device includes classic computer hardware 6 in Harvard or von Neumann architecture (classical hardware). The control device μC of the quantum computer QC is preferably such classical hardware 6. The classical hardware 6 preferably executes classical programs and classical software 5 (classical software, classical algorithms). The control device µC then executes a total of hybrid quantum technology/classical programs and software 3 (Quantum classical hybrid software) of classical data processing and quantum processing. The abstract quantum gate models also include classic control commands for the control device µC, which, as part of the implementation of a quantum gate operation, allow the control device µC to have means for influencing and/or reading out the quantum bits of the quantum dots NV1, NV2, NV3 and the core quantum bits of the core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ in an appropriate manner and to process measurement results and parameters as part of carrying out a quantum gate operation. In this respect, the abstract quantum gate models also represent hybrid software modules, so the boundary here is blurred.

The user then applies the mixed method provided by the control device µC of the quantum computer QC to concrete real-world problems. (Real-world problem and data sets) as part of application programs 2.

The technical teaching of this document claims a method that can be divided into these sub-methods and refers to it with the term quantum computer stack.

The document presented here thus discloses a quantum computer QC, the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ a control device µC with a Memory RAM, NVM and a computer core CPU, means WFG, LDRV, LD, DBS, OS, MW/RF-AWFG, MWA, LH1, LV1, LV2 for influencing the quantum states of the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ , Medium WFG, LDRV, LD, DBS, OS, MW/RF-AWFG, MWA, LH1, LV1, LV2, PD, V for electrically and/or optically reading out the quantum states of the quantum dots NV1, _NV2 , NV3 and core quantum dots CI11, _CI12 , _CI13 , _CI21 , _CI22 , _CI23 , _CI31 , _CI32 , _CI33 . The computer core CPU of the control device µC of the quantum computer QC executes information in the memory RAM, NVM of the control device µC as control commands of the computer core CPU and / or uses these as data. The proposed quantum computer is characterized in that the information in the memory RAM, NVM of the control device µC includes a software stack. The software stack 1 preferably includes, for example, quantum gate hardware models 11, 12 to 17, 22, 23, a transcompiler 9, abstract quantum gate models 8 for the execution of quantum gate operations by the quantum computer QC. The information is preferably present in the memory RAM, NVM of the control device µC as a hybrid quantum technological/classical program 3 in the form of hybrid binary codes, these hybrid binary codes comprising classical binary classical codes for classical algorithms 4 and binary quantum technological codes of quantum algorithms 7. The respective binary quantum technological codes represent respective quantum gate models (8) associated with them. The control device (µC) uses the transcompiler (9) to convert binary quantum technological codes of the quantum gate models (8) of quantum algorithms (7) into sequences of calls to control programs (12 to 17, 22, 23), which the control device µC executes. By executing the relevant control programs (12 to 17, 22, 23) in accordance with the quantum gate hardware models (11), the control device µC sets hardware commands, for example in the form of corresponding signaling, to the means (WFG, LDRV, LD, DBS, OS, MW /RF-AWFG, MWA, LH1, LV1, LV2, PD, V) for influencing and / or reading out the quantum states of the quantum dots NV1, NV2, NV3 and core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ). The control device µC causes the hardware of the quantum computer QC in the form of the said means (WFG, LDRV, LD, DBS, OS, MW/RF-AWFG, MWA, LH1, LV1, LV2, PD, V) to issue these hardware commands 12 to 17 , 22, 23 are preferably carried out in a time-synchronous manner and preferably in the correct phase. The control device µC causes the hardware of the quantum computer QC in the form of the said means WFG, LDRV, LD, DBS, OS, MW/RF-AWFG, MWA, LH1, LV1, LV2, PD, V thus, by executing the relevant control programs 12 to 17, 22, 23 according to the quantum gate hardware models 11, if necessary, the answers of the the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The control device μC thus achieves a quantum computer calculation result through such detection and stores it or outputs it or uses it further.

In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes, at least at times, additional information that the control device (µC) uses to control and/or monitor and/or regulate an energy supply (LDV, TS, BENG, SRG, BENG2, SRG2) of device parts of the quantum computer (QC) is used, this control and / or control and / or regulation of the energy supply (LDV, TS, BENG, SRG, BENG2, SRG2) of device parts of the quantum computer (QC) in parallel or quasi-parallel to the The hardware commands are executed in the form of the control programs (12 to 17, 22, 23).

In a variant of the quantum computer QC, the content of the memory includes RAM, NVM information, in particular a control program 16, which the control device (µC) uses to control and/or control and/or regulate the optical system (OS) of the quantum computer (QC), wherein this control and/or control and/or regulation of the optical system (OS) of the quantum computer (QC) takes place in parallel or quasi-parallel with the execution of the hardware instructions in the form of the control programs (12 to 17, 22, 23). In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes information from a control program 16, which the control device (µC) for controlling and / or monitoring and / or regulating the optical system (OS) of the quantum computer (QC). Dependence on a position measuring system (ClF, CM1).

In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes information, in particular a control program 22, which the control device (µC) for controlling and / or monitoring and / or regulating a positioning device (XT, YT, PV, PVC) used for positioning and/or aligning the substrate (D) relative to the optical system (OS) of the quantum computer (QC) depending on a position measuring system (CIF, CM1), this control and/or control and/or regulation of the control and/or or control and/or regulation of the positioning device (XT, YT, PV, PVC) of the quantum computer (QC) takes place in parallel or quasi-parallel with the execution of the hardware commands in the form of the control programs (12 to 17, 23).

In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes information, in particular a control program 15, which the control device (µC) for controlling and / or monitoring and / or regulating a magnetic field measuring device (MSx, MSy, MSy, MFSx, MFSy, MFSz) for recording the magnetic flux density at the location of the quantum dots (NV1, NV2, NV3) and/or at the location of the core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1, CI2 ₂ , _{CI2 3 ,} CI3 ₁ , CI3 ₂ , CI3 ₃ ) of the quantum computer (QC) is used, this control and/or control and/or regulation of the magnetic field measuring device (MSx, MSy, MSy, MFSx, MFSy, MFSz) of the quantum computer (QC) being temporally parallel or quasi-parallel to The hardware commands are executed in the form of the control programs (12 to 17, 22, 23).

In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes additional information, in particular the control program 15, which the control device (µC) for controlling and / or monitoring and / or regulating a magnetic field generating device (MGx, MGy, MGy, MFSx , MFSy, MFSz) to generate an additional magnetic flux density at the location of the quantum dots (NV1, NV2, NV3) and/or at the location of the core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) of the quantum computer (QC) is used, this control and / or control and / or regulation of the magnetic field generating device (MGx, MGy, MGy, MFSx, MFSy, MFSz) of the quantum computer (QC) in parallel or quasi in time takes place parallel to the execution of the hardware commands in the form of the control programs (12 to 17, 22, 23).

In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes additional information, in particular the control program 15, this control and / or control and / or regulation of the magnetic field generating device (MGx, MGy, MGy, MFSx, MFSy, MFSz ) of the quantum computer (QC) depending on the measured values recorded by the magnetic field measuring device (MSx, MSy, MSy, MFSx, MFSy, MFSz) for detecting the magnetic flux density at the location of the quantum dots (NV1, NV2, NV3) and/or at the location of Core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ ) of the quantum computer (QC) takes place.

In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes information, in particular a control program 23, which the control device (µC) uses to control and/or monitor and/or regulate a cooling device tung (KV, HeCLCS) for cooling the material at the location of the quantum dots (NV1, NV2, NV3) and/or at the location of the core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) of the quantum computer (QC), this control and/or control and/or regulation of the cooling device (KV, HeCLCS) of the quantum computer (QC) being carried out in parallel or quasi-parallel with the execution of the hardware commands in the form of the control programs (12 to 17, 22, 23).

In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes further information, in particular the control program 23, which the control device µC for controlling and / or monitoring and / or regulating and / or a temperature sensor system TS for detecting a temperature measurement value the temperature of the material at the location of the quantum dots (NV1, NV2, NV3) and/or at the location of the core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) of the quantum computer QC is used, the control and / or control and / or regulation of the cooling device (KV, HeCLCS) of the quantum computer QC depending on this temperature measurement value being carried out in parallel or quasi-parallel with the execution of the hardware commands in the form of the control programs (12 to 17, 22, 23).

Based on the previous description, the document presented here describes a quantum computer QC, in which the content of the memory RAM, NVM of the control device µC of the quantum computer QC includes information, in particular a data interface program 28, which the control device µC for control and control one or more data interfaces DBIF of the quantum computer QC is used, this control and control of one or more data interfaces DBIF of the quantum computer QC being carried out in parallel or quasi-parallel with the execution of the hardware commands in the form of the control programs (12 to 17, 22, 23).

In a variant of the quantum computer QC, the content of the memory (RAM, NVM) includes information, in particular a cryptography program 25, which the control device µC uses to encrypt and/or decrypt data that the quantum computer QC and/or the control device µC uses via the Receive or send the DBIF data interface and/or used for the encryption and/or decryption of other data of the quantum computer QC, this encryption and/or decryption being carried out in parallel or quasi-parallel with the execution of the hardware commands in the form of the control programs (12 to 17, 22, 23 ) he follows. In a variant based on this, the control device μC carries out a method for PQC-capable encryption of data by executing the cryptography program 25. This means that this communication is protected from potential attackers and can no longer be easily decrypted. This is particularly important when protecting the control and/or communication of unmanned autonomous vehicles and other mobile objects such as those already described here. In a variant based on this, the control device µC generates, at least temporarily, one or more times an encryption key for the cryptographic program 25 by means of at least one quantum operation with the aid of one or more quantum dots (NV1, NV2, NV3) and/or one or more core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ). In the simplest case, the control device µC sets one or more quantum dots (NV1, NV2, NV3) and/or one or more core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) back, so that preferably all reset quantum bits of the one or more quantum dots (NV1, NV2, NV3) and / or all reset quantum bits of one or more core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) with a 50% probability of independently outputting a logical 1 value or a logical 0 value when reading out. The control device µC of the quantum computer QC1 can use the random number generated in this way as a key for a cryptography method based on a cryptography program 25. The advantage is an unpredictable key for data encryption.

Such a quantum computer QC1 can be used in a quantum computer system QUSYS with one or more further quantum computers QC2 to QC16 and/or one or more conventional computers (ZSE, µC2 to µC16). An external data bus EXTDB preferably connects the one or more quantum computers QC1 to QC16 and/or the one or more conventional computers (ZSE, µC2 to pC16) with one another. The external data bus EXTDB can be fully or partially wired and/or wireless. The one or more quantum computers QC1 to QC16 and/or the one or more conventional computers (ZSE, µC2 to µC16) of the quantum computer system QUSYS can each have one or more data bus interfaces DBIF, so that complex topologies are possible. One or more quantum computers (QC1, QC8, QC9, QC16) can, for example, function as gateways between several QUSYS quantum computer systems.

The technical teaching presented here discloses a quantum computer system QUSYS, the quantum computer system QUSYS comprising at least one quantum computer QC1, as described above. A computer core CPU of the control device μC of the at least one quantum computer QC1 of the quantum computer system QUSYS is preferably connected to the external data bus EXTDB via the data bus interface DBIF. A computer core CPU of the control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS is preferably connected via the data bus interface DBIF and via this external data bus EXTDB to a central control unit ZSE of the quantum computer system QUSYS. The control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS encrypts at least part of the data communication between the central control unit ZSE of the quantum computer system QUSYS Control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS by means of the PQC-capable cryptography program 25. The control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS decrypts at least part of the data communication between the central control unit ZSE of the quantum computer system QUSYS Control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS using the PQC-capable cryptography program 25. This makes it difficult for an attacker to disrupt the quantum computer system QUSYS by manipulating the data transmission between Components of the QUSYS quantum computer system. In this context, this document refers to the exemplary book Daniel J. Bernstein, Johannes Buchmann, Erik Dahmen "Post-Quantum Cryptography" November 19, 2008"Springer; 2009. Edition (November 19, 2008), ISBN-10: 3540887016, ISBN -13:978-3540887010.

The technical teaching presented here discloses a quantum computer system QUSYS, wherein the quantum computer system QUSYS comprises at least one quantum computer QC1, as described above, and comprises at least one further quantum computer QC2, as described above. A computer core CPU of the control device μC of the at least one quantum computer QC1 of the quantum computer system QUSYS is preferably connected to the external data bus EXTDB via the data bus interface DBIF of the at least one quantum computer QC1. A computer core CPU of the control device µC of the further quantum computer QC2 of the quantum computer system QUSYS is preferably connected to the external data bus EXTDB via the data bus interface DBIF of the further quantum computer QC2. A computer core CPU of the control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS is preferably connected via the data bus interface DBIF of the at least one quantum computer QC1 and via this external data bus EXTDB and via the data bus interface DBIF of the further quantum computer QC2 to a computer core CPU of the control device µC of the further quantum computer QC2 of the QUSYS quantum computer system. The control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS encrypts at least part of the data communication between the control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS and the control device µC of the further quantum computer QC2 of the quantum computer system QUSYS by means of the PQC-capable cryptography program 25. The control device µC of the further quantum computer QC2 of the quantum computer system QUSYS encrypts at least part of the data communication between the control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS and the control device µC of the further quantum computer QC2 of the quantum computer system QUSYS by means of the PQC-capable cryptography program 25. The control device µC of the at least a quantum computer QC1 of the quantum computer system QUSYS decrypts at least part of the data communication between the control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS and the control device µC of the further quantum computer QC2 of the quantum computer system QUSYS by means of the PQC-capable cryptography program 25. The control device µC of the further quantum computer QC2 of the quantum computer system QUSYS decrypts at least part of the data communication between the control device µC of the at least one quantum computer QC1 of the quantum computer system QUSYS and the control device µC of the further quantum computer QC2 of the quantum computer system QUSYS by means of the PQC-capable cryptography program 25. This makes it more difficult for an attacker to disrupt the quantum computer system QUSYS Manipulation of data transfer between components of the QUSYS quantum computer system.

Use for environmental exploration

The document presented here proposes a mobile device comprising a QUSYS quantum computing system as described above. The quantum computer system QUSYS preferably comprises at least one quantum computer QC1, QC2, as described above. Preferably, the mobile device has sensors SENS on. These sensors may include, for example, but not only, radar sensors, LIDAR sensors, ultrasonic sensors, camera-based sensors, quantum sensors, sonar sensors and other sensors. The SENS sensors and, if applicable, devices that are connected to the mobile device via wired and/or wireless data connections typically transmit sensor data to the QUSYS quantum computer system. The quantum computer system QUSYS is preferably set up to execute one or more quantum algorithms which increase the performance of SENS sensors and/or which accelerate the processing of the data and the sensor data of the SENS sensors and/or other data.

For example, the mobile device can also be set up to carry out processing and optimization tasks in sensor remote sensing and/or exploration of the earth's surface and/or in sonar exploration and/or in ultrasound exploration and/or in, using at least one quantum computer QC1, QC2 of its quantum computer system QUSYS the image recognition and/or in the image processing and/or the exploration of the water surface and/or in the exploration of a marine volume and/or the airspace and/or the sea area using the SENS sensors and the data.

For example, the mobile device can also be set up to execute quantum computing routines and/or quantum computing methods in the area of radar data processing and/or sonar data processing and/or ultrasound data processing and/or LIDAR data processing using a quantum computer QC1, QC2 of its quantum computer system QUSYS .

For example, the mobile device can also be set up to focus sensor raw data of the received sensor data and/or the data of the sensors SENS using at least one quantum computer QC1, QC2 of its quantum computer system QUSYS.

For example, the mobile device can also be set up to carry out methods of radar interferometry and/or sonar interferometry using at least one quantum computer QC1, QC2 of its quantum computer system QUSYS.

For example, the mobile device can also be set up to generate radar images and/or LIDAR images and/or sonar images and/or images based on the sensor data of the SENS sensors and/or satellite data and/or using at least one quantum computer QC1, QC2 of its quantum computer system QUSYS. or other data to generate and/or evaluate.

The mobile device can be part of a swarm and in particular part of a swarm of such mobile devices and/or part of a swarm of mobile devices, of which at least one mobile device is a mobile device as described above.

The mobile device can be a floating body and/or a robot and/or a land vehicle and/or a vehicle and/or a motor vehicle and/or a two-wheeler and/or a tricycle and/or a truck and/or a commercial vehicle and/or a Transport vehicle and/or a drone and/or a robot drone and/or a missile and/or a floating body and/or a ship drone and/or a submersible body and/or a ship and/or a submarine and/or a submarine -Drone and/or a torpedo and/or a sea mine and/or a landmine and/or a missile and/or a projectile and/or a satellite and/or a space station and/or a spacecraft and/or a trailer and /or a barge and/or a container, in particular a sea container, and/or a smartphone and/or a piece of clothing and/or a piece of jewelry and/or a portable quantum computer system (QUSYS) and/or a mobile quantum computer system (QUSYS) and /or a vehicle and/or a robot and/or an aircraft and/or a spacecraft and/or an underwater vehicle and/or a surface floating body and/or an underwater floating body and/or a mobile medical device and/or a deployable weapon system and/or a warhead and/or a surface or underwater vehicle and/or a projectile and/or a weapon system and/or a gun and/or an ammunition component and/or another mobile device and/or a movable device or include such a device.

List of characters

• 1 shows the quantum computer QC described above in a simplified schematic form.
• 2 shows two exemplary quantum bits QUB1, QUB2.
• 3 shows the block diagram of an exemplary quantum computer QC with an exemplary, schematically indicated three-bit quantum register.
• 4 shows an exemplary quantum computer system QUSYS with an exemplary central control unit ZSE.
• 5 shows the structure of an exemplary software stack, as is the preferred content of the memory RAM, NVM of the control device µC of the quantum computer QC.

Description of the characters

The figures explain the proposal schematically and simplified. The disclosure of the document presented here is not limited to the figures and also includes other combinations.

Figure 1

1 shows the exemplary deployable quantum computer QC described above in a schematically simplified form. The document presented here does not repeat the description at this point.

Figure 2

The 2 shows two exemplary quantum bits QUB1, QUB2. In the following, the document presented here first describes the first quantum bit QUB1. The second quantum bit QUB2 results analogously. The substrate D has a bottom US on which a back contact BSC is attached. The substrate D is particularly preferably made of diamond. The quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ are preferably irradiated with pump radiation LB from the underside US of the substrate D The isotopes of the substrate D preferably have essentially no nuclear magnetic moment μ. An epitaxial layer DEPI is applied to the substrate D to improve the electronic properties. Preferably, the substrate D and/or the epitaxial layer DEPI essentially only comprise isotopes without a nuclear magnetic moment μ. Preferably, the substrate D and/or the epitaxial layer DEPI essentially comprises only one isotope type of an isotope without a nuclear magnetic moment μ. The package consisting of substrate D and epitaxial layer DEPI has a surface OF. A vertical line LV1 is applied to the surface OF as part of an exemplary crossbar structure, through which a vertical electrical current IV1 modulated with a vertical modulation flows. The surface OF and the vertical line LV1 are covered by insulation IS. If necessary, there is further insulation between the vertical line LV1 and the surface OF in order to electrically isolate the vertical line LV1. A first horizontal line LH1 is applied to the insulation IS, through which a first horizontal electrical current IH1, modulated with a first horizontal modulation, flows. The first vertical line LV1 and the first horizontal line LH1 are preferably electrically insulated from each other. Preferably, the angle α ₁₁ between the first horizontal line LH1 and the first vertical line LV1 is a right angle of 90°. The first horizontal line LH1 and the first vertical line LV1 preferably cross above the paramagnetic center of the first quantum dot NV1. The first quantum dot NV1 is preferably an NV center in diamond. The first quantum dot NV1 is preferably located directly below the intersection point of the first horizontal line LH1 with the first vertical line LV1 at a first distance d1 below the surface OF in the epitaxial layer DEPI. The first distance d1 is preferably between 10µm and 20µm, worse between 5µm and 40µm, worse between 2.5µm and 80µm. In the case of diamond as the material of the epitaxial layer DEPI, the first quantum dot NV1 can be, for example, an NV center. The use of SiV and/or TR12 centers and other paramagnetic centers in diamond is also conceivable. If the horizontal modulation of the first horizontal current IH1 is shifted by +/- π/2 compared to the vertical modulation of the first vertical current IV1, then at the location of the first quantum dot NV1, for example, a rotating magnetic field B _NV results, which influences the first quantum dot NV1 . The control device µC of the quantum computer QC can use this to manipulate the first quantum dot NV1. Here, the control device µC selects the frequency so that the first quantum dot NV1 resonates with the rotating magnetic field B _NV . The duration of the pulse then determines the angle of rotation of the quantum information of the first quantum dot NV1. The direction of polarization determines the direction.

The 2 includes, for example, six core quantum dots
firstly, a first core quantum dot CI1 ₁ , which is assigned to the first quantum dot NV1, and
secondly, a second core quantum dot CI1 ₂ , which is assigned to the first quantum dot NV1, and
thirdly, a third core quantum dot CI1 ₃ , which is assigned to the first quantum dot NV1, and
fourthly, a first core quantum dot CI2 ₁ which is assigned to the second quantum dot NV2, and
fifth, a second core quantum dot CI2 ₂ associated with the second quantum dot NV2, and
sixthly, a third core quantum dot CI2 ₃ which is assigned to the second quantum dot NV2.

Each of the core quantum dots forms a core quantum bit with the lines LV1, LH1, LH2. The quantum is in the respective core quantum bit point NV1, NV2 replaced by the core quantum point CI1 ₁ , CI1 ₂ , CI1 ₃ in QUB1 and CI2 ₁ , CI2 ₂ , CI2 ₃ in QUB2.

Isotopes with a magnetic nuclear spin preferably form the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ in the substrate D. In the case of diamond as the material of the epitaxial layer DEPI or the substrate D, a core quantum dot can, for example be a ¹³ C isotope or a nucleus of a nitrogen atom of a NV center.

2 shows an exemplary quantum register with a first quantum bit QUB1 and a second quantum bit QUB2. The quantum bits QUB1, QUB2 of the quantum register have a common substrate D and a common epitaxial layer DEPI. The first vertical line of the first quantum bit QUB1 is the first vertical line LV1 of the second quantum bit QUB2. The first vertical line LV1 and the first horizontal line LH1 preferably cross above the first quantum dot NV1, which is preferably located at a first distance d1 below the surface OF, at a preferably right angle α ₁₁ of 90°. The first vertical horizontal line LV1 and the second horizontal line LH2 preferably cross above the second quantum dot NV2, which is preferably located at a second distance d2 below the surface, at a preferably right angle α ₁₂ . The first distance d1 and the second distance d2 are preferably similar to one another. For NV centers in diamond as quantum dots NV1, NV2, these distances d1, d2 are preferably 10nm to 20nm. A first vertical current IV1 modulated with a horizontal modulation flows through the first vertical line LV1. A first horizontal current IH1 modulated with a first horizontal modulation flows through the first horizontal line LH1. A second horizontal current IH2 modulated with a second horizontal modulation flows through the second horizontal line LH2. The first quantum dot NV1 is spaced from the second quantum dot NV2 by a distance sp12.

The 2 shows an exemplary core-electron core-electron quantum register CECEQUREG.

The core-electron-core-electron quantum register includes an electron-electron quantum register in which the first quantum dot NV1 of the first quantum bit QUB1 can couple with the second quantum dot NV2 of the second quantum bit QUB2.

The core-electron-core-electron quantum register includes a first core-electron quantum register, in which the first quantum dot NV1 of the first quantum bit QUB1 can couple with the first core quantum dot CI1 ₁ of the first core quantum bit.

The core-electron-core-electron quantum register includes a second core-electron quantum register, in which the first quantum dot NV1 of the first quantum bit QUB1 can couple with the second core quantum dot CI1 ₂ of the second core quantum bit.

The core-electron-core-electron quantum register includes a third core-electron quantum register, in which the first quantum dot NV1 of the first quantum bit QUB1 can couple with the third core quantum dot CI1 ₃ of the second core quantum bit.

The core-electron-core-electron quantum register includes a fourth core-electron quantum register, in which the second quantum dot NV2 of the second quantum bit QUB2 can couple with the first core quantum dot CI2 ₁ of the fourth core quantum bit.

The core-electron-core-electron quantum register includes a fifth core-electron quantum register, in which the second quantum dot NV2 of the second quantum bit QUB2 can couple with the second core quantum dot 1, CI2 ₂ of the fifth core quantum bit.

The core-electron-core-electron quantum register includes a sixth core-electron quantum register, in which the second quantum dot NV2 of the second quantum bit QUB2 can couple with the third core quantum dot CI2 ₃ of the sixth core quantum bit.

This is the simplest form of a quantum bus with a first quantum ALU QUALU1 (NV1, CI1 ₁ , CI1 ₂ , CI1 ₃ ) and a second quantum ALU QUALU2 (NV2, CI2 ₁ , CI2 ₂ , CI2 ₃ ). The control device µC can entangle the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ of the first quantum ALU NV1, Cl1 ₁ , CI1 ₂ , CI1 ₃ and the core quantum dots of the second quantum ALU QUALU2 with one another using the first quantum dot NV1 and the second quantum dot NV2. The first quantum dot NV1 and the second quantum dot NV2 are preferably used to transport the dependency and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ are used for calculations and storage. This takes advantage of the fact that the range of coupling of the quantum dots NV1, NV2 with each other is greater than the range of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ with each other and that the T2 time of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ is longer than that of the quantum dots NV1, NV2.

Typically, the distance between the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ of the first quantum ALU QUALU1 and the second quantum dot NV2 is greater than the electron-nucleus coupling range, so that the state of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ of the first quantum ALU QUALU1 cannot influence the state of the second quantum dot NV2 and the state of the second quantum dot NV2 cannot influence the state of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ of the first quantum ALU QUALU1.

Typically, the distance between the core quantum dots CI2 ₁ , CI2 ₂ , CI2 ₃ of the second quantum ALU QUALU2 and the first quantum dot NV1 is greater than the electron-nucleus coupling range, so that the state of the core quantum dots CI2 ₁ , CI2 ₂ , CI2 ₃ of the second quantum ALU QUALU2 cannot influence the state of the first quantum dot NV1 and the state of the first quantum dot NV1 cannot directly influence the state of the core quantum dots CI2 ₁ , CI2 ₂ , CI2 ₃ of the second quantum ALU QUALU2.

2 shows an exemplary quantum register with a second horizontal shielding line SH2 and with a first horizontal shielding line SH1 and with a third horizontal shielding line SH3. The additional shielding lines allow the injection of additional currents to improve the selection of the quantum dots during the execution of the operations by energizing the vertical and horizontal lines. The two additional lines enable even better adjustment.

2 shows an exemplary two-bit electron-electron quantum register with a common first vertical line LV1, several shield lines and two quantum dots NV1, NV2. In the 2 To explain the readout process, a first vertical shielding line SV1 is drawn parallel to the first vertical line LV1. Since this is a cross-sectional image, the corresponding second vertical shielding line SV2, which also runs parallel to the first vertical line LV1 on the other side, is not shown. In this example, the shielding lines are connected to the substrate D via contacts. If an extraction field is now created between two parallel shielding lines by applying an extraction voltage between these shielding lines SV1, SV2, a measurable current flow occurs when the light source LD irradiates the quantum dots NV1, NV2 with pump radiation LB and these are in the correct quantum state. Further information can be found, for example, in Petr Siyushev, Milos Nesladek, Emilie Bourgeois, Michal Gulka, Jaroslav Hruby, Takashi Yamamoto, Michael Trupke, Tokuyuki Teraji, Junichi Isoya, Fedor Jelezko, “Photoelectrical imaging and coherent spin-state readout of single nitrogen-vacancy centers in diamond”, Science 363, 728-731 (2019) 15 February 2019 can be found.

The two quantum dots NV1, NV2 2 are each part of several nuclear-electron quantum registers. Each quantum dot NV1, NV2 is the in the example 2 Part of a respective quantum ALU QUALU1, QUALU2.

The first quantum dot NV1 of the first quantum ALU QUALU1 can be used in the example 2 interact with a first core quantum point Cl1 ₁ of the first quantum ALU QUALU1 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the first horizontal line LH1 and the first vertical line LV1 with a first horizontal current IH1 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with a first electron nuclear radio wave resonance frequency f _RWEC1-1 for the first quantum ALU QUALU1 or a first nuclear electron microwave resonance frequency f _{MWCE1_1} for the first quantum ALU QUALU1. The quantum computer QC measures this first electron-nuclear radio wave resonance frequency f _{RWEC1_1} for the first quantum ALU QUALU1 and this first core-electron microwave resonance frequency (f _{MWCE1_1} ) for the first quantum ALU QUALU1, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The first quantum dot NV1 of the first quantum ALU QUALU1 can be used in the example 2 interact with a second core quantum point CI1 ₂ of the first quantum ALU QUALU1 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the first horizontal line LH1 and the first vertical line LV1 with a first horizontal current IH1 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with _a second electron nuclear radio wave resonance frequency f _{RWEC2_1} for the first quantum ALU _QUALU1 or a second nuclear electron microwave resonance frequency f _{MWCE2_1} for the first quantum ALU QUALU1. The quantum computer QC measures this second electron nuclear radio wave resonance frequency f _{RWEC2_1} for the first quantum ALU QUALU1 and this second nuclear elect ron microwave resonance frequency (f _{MWCE2_1} ) for the first quantum ALU QUALU1 preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The first quantum dot NV1 of the first quantum ALU QUALU1 can be used in the example 2 interact with a third core quantum point CI1 ₃ of the first quantum ALU QUALU1 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the first horizontal line LH1 and the first vertical line LV1 with a first horizontal current IH1 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with a third electron nuclear radio wave resonance frequency f _{RWEC3_1} for the first quantum ALU QUALU1 or a third nuclear electron microwave resonance frequency f _{MWCE3_1} for the first quantum ALU QUALU1. The quantum computer QC measures this third electron-nuclear radio wave resonance frequency f _{RWEC3_1} for the first quantum ALU QUALU1 and this third core-electron microwave resonance frequency (f _{MWCE3_1} ) for the first quantum ALU QUALU1, preferably in an _{initialization} step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The second quantum dot NV2 of the second quantum ALU QUALU2 can be used in the example 2 interact with a first core quantum point CI2 ₁ of the second quantum ALU QUALU2 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the second horizontal line LH2 and the first vertical line LV1 with a second horizontal current IH2 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with a fourth electron nuclear radio wave resonance frequency f _{RWEC1_2} for the second _quantum ALU _QUALU2 or a fourth nuclear electron microwave resonance frequency f _{MWCE1_2} for the second quantum ALU QUALU2. The quantum computer QC measures this fourth electron-nuclear radio wave resonance frequency f _RWEC1-2 for the second quantum ALU QUALU2 and this fourth core-electron microwave resonance frequency (f _MWCE1-2 ) for the second quantum ALU QUALU2, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The second quantum dot NV2 of the second quantum ALU QUALU2 can be used in the example 2 interact with a second core quantum point CI2 ₂ of the second quantum ALU QUALU2 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the second horizontal line LH2 and the first vertical line LV1 with a second horizontal current IH2 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with _a fifth electron nuclear radio wave resonance frequency f _{RWEC2_2} for the second quantum ALU QUALU2 or a fifth nuclear electron microwave resonance frequency f _{MWCE2_2} for the second quantum ALU QUALU2. The quantum computer QC measures this fifth electron-nuclear radio wave resonance frequency f _{RWEC2_2} for the second quantum ALU QUALU2 and this fifth core-electron microwave resonance frequency (f _{MWCE2_2} ) for the second quantum ALU QUALU2, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The second quantum dot NV2 of the second quantum ALU QUALU2 can be used in the example 2 interact with a third core quantum point CI2 ₃ of the second quantum ALU QUALU2 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the second horizontal line LH2 and the first vertical line LV1 with a second horizontal current IH2 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with _a sixth electron nuclear radio wave resonance frequency f _{RWEC2_2} for the second quantum ALU QUALU2 or a sixth nuclear electron microwave resonance frequency f _{MWCE3_2} for the second quantum ALU QUALU2. The quantum computer QC measures this sixth electron nucleus radio wave resonance frequency f _RWEC3 _ ₂ for the second quantum ALU QUALU2 and this sixth Nuclear electron microwave resonance frequency (f _{MWCE3_2} ) for the second quantum ALU QUALU2 preferably in an initialization step once by _an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

Since the coupling range of the quantum dots NV1, NV2 is greater, they can be coupled to one another. The second quantum dot NV2 of the second quantum ALU QUALU2 can in the example 2 interact with the first quantum dot NV1 of the first quantum ALU QUALU1 when the microwave and/or radio wave frequency generator MW/RF-AWFG supplies the first horizontal line LH1 and the second horizontal line LH2 and the first vertical line LV1 with a first horizontal current IH1 and a second horizontal current IH2 and a first vertical current IV1, which the microwave and / or radio wave frequency generator MW / RF-AWFG with an electronl-electron2 microwave resonance frequency f _MWEE12 for the coupling of the first quantum dot NV1 of the first quantum ALU QUALU1 with the second quantum dot NV2 modulated the second quantum ALU QUALU2. The computer core CPU of the quantum computer QC measures this electron-electron2 microwave resonance frequency f _MWEE12 for the coupling of the first quantum dot NV1 of the first quantum ALU QUALU1, preferably once in the said initialization step by another OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory RAM, NVM of the computer core CPU of the control device µC, which this computer core CPU retrieves when the corresponding electron-electron quantum register comprising the first quantum dot NV1 and the second quantum dot NV2 are controlled should. The computer core CPU of the control device µC then sets the frequencies accordingly.

Figure 3

3 shows the block diagram of an exemplary quantum computer QC with an exemplary, schematically indicated three-bit quantum register, which could possibly also be replaced, for example, by a three-bit core-electron-core-electron quantum register (CECEQUREG) with three quantum ALUs. An extension to an n-bit quantum register is easily possible for a person skilled in the art.

The core of the exemplary control device 3 is a control device μC which preferably includes a computer core CPU. The overall device preferably has a magnetic field control, preferably in the form of a first magnetic field control MFSx and a second magnetic field control MFSy and a third magnetic field control MFSz, which preferably receives its operating parameters from said control device µC and preferably returns operating status data to this control device µC. The magnetic field control MFSx, MFSy, MFSz is preferably a multi-dimensional controller whose task is to compensate for an external magnetic field through active counter-control. For this purpose, the magnetic field control MFSx, MFSy, MFSz preferably uses one or more magnetic field sensors MSx, MSy, MSZ, which preferably monitor the magnetic flux in the quantum computer QC, preferably in the vicinity of the quantum dots NV1, NV2, NV3 and those not shown in the figure for a better overview Core quantum _dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 1 , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ were recorded. The magnetic field sensors MSx, MSy, MSZ are preferably quantum sensors. Here is an example of the registrations DE 10 2018 127 394.0 , DE 10 2019 130 114.9 , DE 10 2019 120 076.8 and DE 10 2019 121 137.9 referred. With the help of the magnetic field control device, for example in the form of the first magnetic field generating means MGx and the second magnetic field generating means MGy and the third magnetic field generating means MGz and, the magnetic field control MFSx, MFSy, MFSz regulates the magnetic flux density B in the vicinity of the quantum dots NV1, NV2, NV3 and not in the core _quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 1 , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ drawn in the figure for a better overview. The document presented here suggests that quantum sensors should preferably be used as magnetic field sensors MSx, MSy, MSZ, since these have the higher accuracy in order to sufficiently stabilize the magnetic field.

The control device µC preferably controls the horizontal and vertical driver stages HD1, HD2, HD3 via a control unit A CBA, which preferably energize the horizontal lines LH1, LH2, LH3 and vertical lines LV1 with the respective horizontal and vertical currents and the correct frequencies and timing Generate burst durations and burst positions based on a temporal starting point t ₀ .

The control unit A CBA sets the frequency and the pulse duration of the first horizontal shielding current ISH1 for the first horizontal shielding line SH1 in the first horizontal driver stage HD1 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the second horizontal shielding current ISH2 for the second horizontal shielding line SH2 in the first horizontal driver stage HD1 and in the second horizontal driver stage HD2 in accordance with the specifications of the control device µC.

The control unit A CBA sets the frequency and the pulse duration of the third horizontal shielding current ISH3 for the third horizontal shielding line SH3 in the second horizontal driver stage HD2 and in the third horizontal driver stage HD3 in accordance with the specifications of the control device µC.

The control unit A CBA sets the frequency and the pulse duration of the fourth horizontal shielding current ISH4 for the fourth horizontal shielding line SH4 in the third horizontal driver stage HD3 and in the fourth horizontal driver stage HD4, which is only indicated due to lack of space, in accordance with the specifications of the control device µC.

The control unit A CBA sets the frequency and the pulse duration of the first horizontal current IH1 for the first horizontal line LH1 in the first horizontal driver stage HD1 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the second horizontal current IH2 for the second horizontal line LH2 in the second horizontal driver stage HD2 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the third horizontal current IH3 for the third horizontal line LH3 in the third horizontal driver stage HD3 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the first vertical shielding current ISV1 for the first vertical shielding line SV1 in the first vertical driver stage HV1 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the first vertical current IV1 for the first vertical line LV1 in the first vertical driver stage VD1 in accordance with the specifications of the control device μC.

Synchronized by the control unit A CBA, these driver stages VD1, HD1, HD2, HD3, HD4 feed their current into the lines SV1, LV1, SV2, SH1, LH1, SH2, LH2, SH3, LH3 in a fixed phase ratio based on a common synchronization time, SH4 on.

The following device elements of the proposed quantum computer QC are for electronic reading of the quantum states of the quantum dots NV1, NV2, NV3 or the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ necessary.

A control unit B CBB is connected to the control device µC via the control data bus SDB. The control device configures the control unit B CBB via the control data bus SDB and sets operating parameters and reads out data and operating states via the control data bus SDB. The control unit B CBB preferably detects the respective photocurrent that the receiver stages HS1, HS2, HS3, VS1 detect and makes the measurement data available to the control device µC via the control data bus SDB.

Previously, the control device µC configures a first horizontal receiver stage HS1 via the control data bus SDB and typically via the control unit B CBB in such a way that it takes the currents fed in by the first horizontal driver stage HD1 again on the other side of the lines.

The control device µC previously configures a second horizontal receiver stage HS2 via the control data bus SDB and typically via the control unit B CBB, preferably in such a way that it takes the currents fed in by the second horizontal driver stage HD2 again on the other side of the lines.

Previously, the control device µC configures a third horizontal receiver stage HS3 via the control data bus SDB and typically via the control unit B CBB in such a way that it takes the currents fed in by the third horizontal driver stage HD3 again on the other side of the lines.

Previously, the control device µC configures a first vertical receiver stage VS1 via the control data bus SDB and typically via the control unit B CBB in such a way that it takes the currents fed in by the first vertical driver stage VD1 on the other side of the lines.

Furthermore, the exemplary system of 3 a light source LD for pump radiation LB in the sense of this document. Using a light source driver LDRV, the control device µC can irradiate the quantum dots NV1, NV2, NV3 with the pump radiation LB via the optical system OS. When irradiated with this pump radiation LB, the paramagnetic centers of the quantum dots NV1, NV2, NV3 produce photoelectrons which pass through the first horizontal receiver stage HS1 and/or the second horizontal receiver stage HS2 and/or the third horizontal receiver stage HS3 and/or the first vertical receiver stage VS1 can be extracted by applying an extraction field, for example to the connected shielding lines SH1, SH2, SH3, SH4, SV1, SV2.

The microwave and/or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms (English: arbitrary wave form generator) includes in the example the 3 the control unit A CBA, the first horizontal driver stage HD1, the second horizontal driver stage HD2, the third horizontal driver stage HD2 and the first vertical driver stage VD1.

In addition, the microwave and/or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms (Arbitrary Wave Form Generator) can also be understood in such a way that in the example of 3 the control unit B CBB, the first horizontal receiver stage HS1, the second horizontal receiver stage HS2, the third horizontal receiver stage HS2 and the first vertical receiver stage VS1.

The lines SV1, LV1, SV2, SH1, LH1, SH2, LH2, SH3, LH3, SH4 form the in the example 3 the exemplary microwave and/or radio wave antenna mWA.

Figure 4

4 shows an exemplary quantum computer system QUSYS with an exemplary central control unit ZSE. In this example, the exemplary central control unit ZSE is connected to a large number of quantum computers QC1 to QC16 via a preferably bidirectional data bus, the external data bus EXTDB. Such a quantum computer system QUSYS preferably includes more than one quantum computer QC1 to QC16. In the example of the 4 Each of the quantum computers QC1 to QC16 includes a control device µC1 to µC16. The quantum computer system QUSYS preferably comprises a charging device LDV, which charges an energy reserve BENG with the energy from a power supply PWR of the charging device LDV and/or supplies an energy processing device SRG with electrical energy. The energy processing device SRG supplies one or more device parts of the quantum computer system QUSYS with electrical energy from the energy reserve BENG and/or with electrical energy from the charging device LDV. The energy processing device SRG preferably supplies one or more device parts of the quantum computer system QUSYS with electrical energy from the energy reserve BENG when a device part of the quantum computer system QUSYS performs a quantum operation for manipulating a quantum dot NV1, NV2, NV3 and/or for manipulating a core quantum dot Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ executes. In the example of the 4 For example, 16 quantum computers QC1 to QC16 are connected to the central control device ZSE via the external data bus EXTDB. The external data bus EXTDB can be any suitable data transmission system. For example, it can be wired, wireless, fiber optic, optical, acoustic, radio-based. In the case of a wired system, the external data bus EXTDB can be, for example, a single-wire data bus, such as a LIN bus, or a two-wire data bus, such as a CAN data bus, in whole or in sections. The external data bus EXTDB can, for example, be a more complex data bus with several conductors and/or several logical levels, etc. in whole or in sections. The external data bus EXTDB can be an Ethernet data bus, for example, in whole or in sections. The external data bus EXTDB can consist entirely of one type of data bus or be composed of various data transmission routes of different types. The external data bus EXTDB can be star-shaped as in the example 4 be arranged. The external data bus EXTDB can be designed in whole or in part, for example as in a daisy chain (https://de.wikipedia.org/wiki/Daisy_Chain) as a chain of bus nodes in the form of the quantum computers QC1 to QC16, in which case each one is preferred the control devices of the quantum computers in question of this part of the quantum computer system QUSYS preferably have more than one data interface in order to be able to connect more than one external data bus EXTDB to the quantum computer in question, for example for such a chain. It is conceivable that one or more quantum computers QC1 to QC16 then act as bus masters and thus as central control devices ZSE for subordinate sub-networks of the QUSYS quantum computer system.

It is therefore also conceivable that the central control device ZSE of the quantum computer system QUSYS is the control device µC of a quantum computer QC or that the central control device ZSE of the quantum computer system QUSYS is a quantum computer. Computer QC with a control device µC, here in the case of 4 The emphasis is on the “normal” computer properties of the control device µC, which controls the quantum computer system QUSYS as the central control device ZSE. From the perspective of the quantum computers QC1 to QC16, the central control device ZSE corresponds to an external monitoring computer of the quantum computer system QUSYS.

The data transmission network of the quantum computer system QSYS can correspond entirely or in parts to a linear chain of bus nodes in the form of the quantum computers QC1 to QC16 along part of the external data bus EXTDB or along the external data bus EXTDB, which can also be closed to form a ring (keyword token ring). .

The data transmission network of the quantum computer system QSYS can be in whole or in part a star structure of bus nodes in the form of the quantum computers QC1 to QC16, which are connected to one or more data lines and/or data transmission media. A star structure is present, for example, when data is transmitted via radio. One, several or all of the quantum computers QC1 to QC16 can also be connected to the central control device ZSE via a point-to-point connection. In this case, the central control device ZSE must have a separate data interface for each point-to-point connection.

The data transmission network of the quantum computer system QSYS can be designed as a tree structure, whereby individual quantum computers, for example, have more than one data bus interface and can serve as a bus master, i.e. central control device ZSE for the sub-network of the data transmission network made up of data buses and quantum computers.

The quantum computer system QUSYS can thus be structured hierarchically, with the control devices μC of individual quantum computers being the central control device ZSE of sub-quantum computer systems. The sub-quantum computer systems are themselves QUSYS quantum computer systems. The central control device ZSE of the sub-quantum computer system is preferably itself a quantum computer, which itself is preferably part of a higher-level quantum computer system QUSYS.

This hierarchy allows different calculations to be processed in parallel in different sub-quantum computer systems, with the number of quantum computers used being chosen differently depending on the task.

The quantum computer system QUSYS therefore preferably comprises several computer units coupled to one another. The computer units are typically computer cores CPU of the control devices µC of the quantum computers QC1 to QC16. Such a computing unit can use an artificial intelligence program that can be coupled to the quantum computers and/or the quantum registers and/or the quantum bits. Both the input into the artificial intelligence program can depend on the state of the quantum dots of these components of the quantum computer system, and the control of the quantum bits and quantum dots of these components of the quantum computer system can depend on the results of the artificial intelligence program. The artificial intelligence program can be executed both in the central control device ZSE and in the control devices µC1 to µC16 of the quantum computers QC1 to QC16. Here, only parts of the artificial intelligence program in which the central control device ZSE can be executed, while other parts of the artificial intelligence program can be executed in the control devices µC of quantum computers within the quantum computer system. Also, only parts of the artificial intelligence program can be executed in one of the control devices µC1 to µC16 of the quantum computers QC1 to QC16, while other parts of the artificial intelligence program are executed in other control devices µC1 to µC16 of other quantum computers QC1 to QC16 within the quantum computer system QUSYS become. This processing of an artificial intelligence program can therefore be distributed over the quantum computer system QUSYS or can be concentrated in a control device of the control devices µC1 to µC16 of the quantum computers QC1 to QC16. The artificial intelligence program works together with quantum points NV1, NV2, NV3 of the quantum computers QC1 to QC16. The control device can actually also be a system of control devices µC1 to µC16. A control device can include, for example, the central control device ZSE of a quantum computer system QSYS with one or more quantum dots NV1, NV2, NV3 and / or one or more control devices µC of one or more quantum computers QC1 to QC16, each with one or more quantum dots NV1, NV2, NV3 . More complex topologies with additional intermediate computer nodes and data bus branches are conceivable. The control device, which as described can also be a combination of control devices, executes an artificial intelligence program. Such a program of artificial For example, intelligence can be a neural network model with neural network nodes.

For example, one or more of the control devices of the control devices µC1 to µC16, the quantum computers QC1 to QC16 and/or the central control unit ZSE can execute a machine learning method. The paper presented here refers, for example, to Akinori Tanaka, Akio Tomiya, Koji Hashimoto, “Deep Learning and Physics (Mathematical Physics Studies)” February 21, 2021, publisher: Springer; Is ed. 2021 Edition, ISBN-10: 9813361077, ISBN-13: 978-9813361072 and Ovidiu Calin, “Deep Learning Architectures: A Mathematical Approach (Springer Series in the Data Sciences),” Springer; 1st ed. 2020 Edition (February 14, 2021), ISBN-10: 3030367231, ISBN-13: 978-3030367237. The procedures explained in these documents are part of the disclosure of the document presented here, provided that a quantum computer carries out QC as described in the document presented here. One of the most common techniques in artificial intelligence that a proposed quantum computer QC and/or a proposed quantum computer system QUSYS can perform is machine learning. Machine learning is a self-adaptive algorithm that a proposed quantum computer QC and/or a proposed quantum computer system QUSYS can execute. The so-called deep learning that a proposed quantum computer QC and/or a proposed quantum computer system QUSYS can execute is typically a subset of machine learning. A proposed quantum computer QC and/or a proposed quantum computer system QUSYS use a series of hierarchical layers or a hierarchy of concepts in machine learning to carry out the machine learning process. The proposed quantum computer QC or the proposed quantum computer system QUSYS preferably use a model of artificial neural networks that are virtually organized and constructed like the human brain. The virtual neurons of the neural network model, which the proposed quantum computer QC or the proposed quantum computer system QUSYS executes, are preferably virtually connected to one another like a network. The first virtual layer of the neural network, the visible input layer, processes raw data input, such as the individual pixels of an image. Data input contains variables accessible to observation, hence “visible layer”. This first virtual layer of the neural network model forwards its outputs to the next virtual layer of the network model when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. This second virtual layer processes the information from the previous virtual layer and also passes on the result when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. The next third virtual layer of the neural network model receives the information of the second virtual layer when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. The third virtual layer of the neural network model further processes this information when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. These layers are called hidden layers. The features they contain are becoming increasingly abstract. Their values are not specified in the original data. Instead, when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS, the neural network model should preferably determine which concepts are useful for explaining the relationships in the observed data. This now continues across all virtual levels of the artificial neural network model. The result is output in the visible last virtual layer when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. This breaks down the desired complicated data processing into a series of nested simple mappings, each describing a different layer of the neural network model.

The neural network model typically uses one or more input values and/or one or more input signals. The neural network model typically provides one or more output values and/or one or more output signals. It is now proposed here to supplement the artificial intelligence program with a program that carries out one or more of the above-mentioned quantum operations on one or more quantum computers of the quantum computers QC1 to QC16. This coupling CAN, FOR EXAMPLE, happen in one direction by driving one or more quantum dots QC1 to QC16. in particular by means of horizontal lines LH1, LH2, LH3 and/or vertical lines LV1, from one or more output values and/or one or more output signals of the neural network model. In the other direction, states of one or more quantum dots are read out at a time and used as input in the artificial intelligence program, in this example the neural network model. The value of one or more input values and/or one or more input signals of the artificial intelligence program, here the neural network model, then depends on the state of one or more of the quantum dots NV1, NV2, NV3 and/or one or more core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , CI33 from.

Figure 5

5 shows the structure of an exemplary software stack 1, as it is the preferred content of the memory RAM, NVM of the control device μC of the quantum computer QC in the form of information.

An application program 2 of the proposed quantum computer QC typically includes hybrid quantum technology/classical programs and software 3.

The hybrid quantum technology/classical programs and the software 3 typically include classical algorithms 4. These classical algorithms 4 are typically located in the form of classical programs and software 5 in the memories RAM, NVM of the control device µC of the quantum computer QC. These programs and software 5 in the RAM, NVM memories of the control device µC of the quantum computer QC are typically in the form of binary codes that encode the classic hardware instructions that the classic computer hardware 6, especially in von Neumann or Harvard architecture, then executes . The classic computer hardware 6, especially in von Neumann or Harvard architecture, is preferably the computer core CPU of the control device µC of the quantum computer QC.

The classic programs and software 5 can, for example, include, in addition to other software components that are required by the control device µC to solve the problem of the application program 2, for example a cryptography program 25 that the control device µC uses for communication and for encrypting and/or decrypting Data that the quantum computer QC and/or the control device µC receives or sends via the data interface DBIF, and/or is used to encrypt and/or decrypt other data from the quantum computer QC. Preferably, the method that the control device uses when executing the cryptographic program 25 is a PQC-secure cryptographic method. The binary-coded classic commands of the cryptography program 25 for the computer core CPU of the control device µC are preferably part of the contents of the RAM, NVM memories of the control device µC of the quantum computer QC.

For data communication with other quantum computers QC1 to QC16 and/or other computer systems, for example a central control unit ZSE, the control device preferably executes a data interface program 28 for controlling and monitoring one or more data interfaces DBIF. The binary-coded classic commands of the data interface program 28 for the computer core CPU of the control device µC are preferably part of the contents of the RAM, NVM memories of the control device µC of the quantum computer QC.

The classic programs and software 5 can, for example, include, in addition to other software components that are required by the control device µC to solve the problem of the application program 2, for example a vehicle condition determination program 27, which the control device µC uses for the position assessment of the overall condition of the vehicle and/or the The vehicle's surroundings are used depending on measured values. The binary-coded classic commands of the vehicle status determination program 27 for the computer core CPU of the control device µC are preferably part of the contents of the RAM, NVM memories of the control device µC of the quantum computer QC.

For example, the vehicle status determination program 27 may include calling a data interface program 28 for controlling and monitoring one or more data interfaces DBIF. The binary-coded classic commands of the data interface program 28 for the computer core CPU of the control device µC are preferably part of the contents of the RAM, NVM memories of the control device µC of the quantum computer QC.

For example, the vehicle condition determination program 27 can include the call to one or more measured value acquisition programs 26 to query the measured values and to control and monitor the associated measuring systems and/or sensors SENS. The quantum computer QC evaluates the sensor data from the SENS sensors. Typically, at least temporarily, states of one or more quantum dots (NV1, NV2) depend directly or indirectly on the values of the sensor data from the SENS sensors, in particular after processing by the computer core CPU or another data processing system. The binary coded classic commands of the Measurement acquisition programs 26 for the computer core CPU of the control device µC are preferably part of the contents of the RAM, NVM memories of the control device µC of the quantum computer QC.

The hybrid quantum technological/classical programs and the software 3 typically include quantum technological algorithms 7. Quantum technological algorithms 7 are typically characterized in that they contain the quantum state of at least one or more of the quantum dots NV1, NV2, NV3 and/or the quantum state of one or more core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 1, Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ changes and/or manipulates and/or reads _.

The quantum technological algorithms 7 preferably include abstract quantum gate models 8. These quantum gate models 8 are preferably present within the quantum technological algorithms 7 as binary coded quantum technological commands. The binary coded quantum technology commands quantum technology algorithms 7 encode the execution commands quantum operations and quantum gates according to the quantum gate models 8. These binary coded quantum technology commands are preferably part of the content of the memories RAM, NVM of the control device µC of the quantum computer QC.

The information in the memory RAM, NVM of the control device µC of the quantum computer QC preferably includes classic instructions and commands for the computer core CPU of the control device µC of the quantum computer QC, which are the program data of a transcompiler 9 with an optimizer and quantum error correction function. The control device μC of the quantum computer QC typically executes this transcompiler 9. By executing the transcompiler 9, the control device µC identifies the binary coded quantum technology commands of the currently processed quantum technology algorithm 7 and assigns the corresponding quantum gate models 8 to them. Depending on the identified quantum gate model 8 for a quantum gate, the control device then possibly executes one or more control programs of the control programs (12 to 17, 22, 23). The quantum computer QC preferably executes the control programs of the control programs (12 to 17, 22, 23) in a time-synchronized manner. For this reason, the control device _µ C preferably programs the means (WFG, LDRV, LD, DBS, OS, MW/RF-AWFG, MWA, LH1, LV1, LV2, PD, V) for influencing and/or reading out the quantum states of the quantum dots (NV1, NV2, NV3) and core quantum dots (Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ ) and then signals to all means (WFG, LDRV, LD, DBS, OS, MW/RF-AWFG, MWA, LH1, LV1, LV2, PD, V) for influencing and / or reading out the quantum states of the quantum dots (NV1, NV2, NV3) and core quantum dots (Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3s) the start of performing a quantum gate operation in the form of a quantum gate, so that these means (WFG, LDRV, LD, DBS, OS, MW/RF- AWFG, MWA, LH1, LV1, LV2, PD, V) for influencing and / or reading out the quantum states of the quantum dots (NV1, NV2, NV3) and core quantum dots (C11 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , C13 ₃ ) the corresponding quantum gate preferably executes autonomously. The control computer µC of the quantum computer QC preferably optimizes the execution of the quantum technological algorithm 7 and the execution of the corresponding quantum gate model 8. Typically, the control computer µC of the quantum computer QC carries out error correction of any quantum computer calculation results obtained in this context using subprograms of the transcompiler 9. The binary, typically classical binary instruction codes of the transcompiler 9 are typically part of the contents of the memories RAM, NVM of the control device μC of the quantum computer QC.

The control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 typically include a control program 12 for monitoring and controlling the one or more microwave and/or radio wave frequency generators MW/RF-AWFG for generating an electromagnetic wave field by means of one or more microwave and / or radio wave antenna mWA, in particular vertical lines LV1, LV2 or horizontal lines LH1 at the respective location of the quantum dots NV1, NV2, NV3, to influence the quantum states of the quantum dots NV1, NV2, NV3 of the quantum computer QC and / or the quantum states of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC.

The control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 typically include an SPc laser control program 13 for the control and control of the waveform generator WFG and the light source driver LDRV and thus the light source LD for the generation of light pulses the waveform generator WFG and the light source driver LDRV and the light source LD.

The control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 typically include a control program 14 for controlling the reading of the quantum states of the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum en points Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 _{1 , Cl2 2 ,} Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC by means of the control device µC. It is preferably a control program 14 for controlling, monitoring and reading out values of the means PD, V for optically reading out the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots _Cl11 , _Cl12 , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 _{3, Cl3 1 ,} Cl3 ₂ , Cl3 ₃ of the quantum computer QC by the control device µC and/or a control program 14 for controlling the control and reading out of values of the means for electrically reading out the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC.

The control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 typically include a control program 15 for detecting the magnetic flux density B in the area of the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC using magnetic field sensors MSx for the magnetic flux density B _x in the direction of the X-axis and/or using magnetic field sensors MSy for the magnetic flux density B _y in the direction of the Y-axis and/or by means of magnetic field sensors MSz for the magnetic flux density B _z in the direction of the Z-axis and/or for controlling and monitoring magnetic field controls MFSx, MFSy, MFSz and/or for controlling and Control of magnetic field generating means MGx, MGy, MGz.

The control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 typically include a control program 16 for controlling the optical system OS in order to optimize the irradiation of the laser beam LB into the substrate D if necessary. This can be, for example, the setting of the focus and/or the setting of apertures.

The control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 typically include a control program 17 for execution by the control device μC and for controlling and setting DC current levels and/or DC voltage levels to influence certain ones Quantum dots NV1, NV2, NV3 of the quantum computer QC and/or certain core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC in such a way that they may be .not participate in a hardware operation or take part in a hardware operation.

The control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 typically include a position control program 22 for checking and controlling a positioning device XT, YT for positioning and, if necessary, aligning the substrate D with respect to the optical system OS.

The control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 typically include a temperature control program 23 for controlling one or more cooling devices KV and/or one or more closed loop helium gas cooling systems HeCLCS.

The binary, typically classical binary command codes of the control programs (12 to 17, 22, 23) of the quantum gate hardware model 11 are typically part of the contents of the memories RAM, NVM of the control device μC of the quantum computer QC.

The software stack in the sense of the document presented here therefore includes a hardware part 20 of the software stack 1 and a software part 19 of the software stack 1. Among other things, in the means (WFG, LDRV, LD, DBS, OS, MW/RF-AWFG, MWA, LH1, LV1, LV2, PD, V) for electrical and/or optical reading of the quantum states of the quantum dots (NV1, NV2, NV3) and core quantum dots (Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ ) and the means (XT, YT) for aligning and positioning the substrate D relative to the optical system OS and in the means (ST, KV, HeCLCS) for detecting, Setting and regulating the temperature overlaps the hardware part 20 of the software stack 1 and a software part 19 of the software stack 1.

In addition, the software stack 1 in the sense of the document presented here includes further exemplary hardware parts (DBIF, vehicle functions, SENS) of the quantum computer QC and other associated software parts (4, 5, 25, 27, 28, 24, 26) software Part 19 of the software stack 1.

The quantum technological algorithms 7, the abstract quantum gate models 8 and the transcompiler 9 with optimizer and quantum error correction are preferably typical quantum technological components of the software part 19 of the software stack 1.

The application programs 2 and the hybrid quantum technology/classical programs and software 3 are typically hybrid components of the software stack 1.

Figure 6

6 shows an aircraft FZ with several deployable quantum computers QC1, QC2. In the example of the 6 the exemplary aircraft FZ has a first quantum computer QC1 and a second quantum computer QC2 and a central control unit ZSE, which is connected to the exemplary two quantum computers QC1, QC2 via an external data bus EXTDB. The external data bus EXTDB is the preferred part of the proposed aircraft FZ. The deployable quantum computers QC1, QC2 preferentially solve NP-hard problems in the proposed aircraft FZ.

• • https://de.wikipedia.org/wiki/NP_(Komplexit%C3%A4tsklasse) und
• • https://en.wikipedia.org/wiki/NP-hardness

For more information on NP-hard problems, see for example

• • https://de.wikipedia.org/wiki/NP_(Komplexit%C3%A4tsklasse) and
• • https://en.wikipedia.org/wiki/NP-hardness

Such problems can, for example, concern the arrangement of certain loads in the cargo hold or optimization problems such as the optimal travel route. It is also conceivable that the deployable quantum computers QC1, QC2 in the aircraft FZ carry out or support artificial intelligence tasks. The deployable quantum computers QC1, QC2 are preferably connected via the external data bus EXTDB to the central control device ZSE, which is typically another control device of the aircraft FZ. For example, the central control device ZSE can be a computer system in the cockpit of the aircraft FZ or in a server room of the aircraft FZ. The proposed aircraft FZ thus preferably comprises a quantum computer system QUSYS with at least one quantum computer QC1, QC2.

The quantum computers QC1, QC2 can also support the pilots and the other computer systems of the FZ aircraft. For example, the quantum computers QC1, QC2 of the aircraft FZ can support the flight attitude control system FLR and/or the navigation system and the autopilot NAV or can take over their function in whole or in part. Of course, the functions of a quantum computer QC are not limited to these functions of an aircraft FZ.

• Airborne Weather Radar

For example, the following come into question:

• Airborne Weather Radar

The evaluation of the Airborne Weather Radar: The weather radar is usually installed in the nose behind a radome, a closed protective cover (radar nose), of the FZ aircraft. It determines the weather in the area. The weather radar can transmit data to one or more quantum computers QC1, QC2 via the external data bus EXTDB. The quantum computers QC1, QC2 can then evaluate the data from the weather radar. The quantum computers QC1, QC2 preferably receive further data, for example via radio interfaces of the aircraft FZ, from other places, such as weather services, airline headquarters, aircraft manufacturers, etc. Typical NP complete problems that can be solved particularly well with quantum computers QC in this context are the evaluation of Weather data and the optimization of the flight route in terms of danger, flight time, costs, etc. The quantum computers QC1, QC2 can carry out these calculations of complete problems and warn the pilots of dangerous weather phenomena at an early stage and make suggestions for optimization. If necessary, the aircraft's conventional computer systems can once again verify the results of the quantum computer programs that were executed on the quantum computers QC1, QC2 in a conventional manner, since then no optimization search is necessary, and confirm to the pilots the correctness of the quantum computer calculation. The document presented here refers to this as an example 10 .

ECAM (Electronic Centralized Aircraft Monitoring) or EICAS (Engine Indication and Crew Alerting System)

Another possible application is, for example, support for the ECAM (Electronic Centralized Aircraft Monitoring) by the quantum computers QC1, QC2 of the aircraft's quantum computer system QUSYS. This electronic system preferably displays the most important engine parameters in the aircraft and checks all aircraft systems, such as fuel and hydraulics. It reports errors and provides information on how to resolve the problem. This electronic system typically displays the most important engine parameters in the FZ aircraft and checks all aircraft systems, such as fuel and hydraulics. It reports suspected or detected errors and provides information on how to resolve the problem. For this purpose, the quantum computers QC1, QC2 can carry out quantum computer calculations in order to be able to recognize the probabilities of critical combinations of aircraft and environmental parameters and to determine measures, sequences of measures and flight routes, etc. in such a way that the probability of critical situations is minimized with maximum effectiveness.

TCAS (Traffic Alert and Collision Avoidance System)

The TCAS is an on-board early warning system of the proposed aircraft FZ to avoid aircraft collisions in the air. If two aircraft are on a collision course, it recommends that both pilots take suitable evasive maneuvers to avert an impending collision. The quantum computers QC1, QC2 can, for example, taking into account the weather conditions, etc., suggest alternative courses that, firstly, have a minimal probability of collision and, secondly, are also optimal with regard to the weather conditions.

Figure 7

Figure 7a

7a shows another example of the use of the proposed deployable quantum computer QC in an aircraft FZ. In the example of the 7a it is a military aircraft FZ. A military aircraft may, for example, be an interceptor, a long-range bomber, or a general combat aircraft, or a helicopter, or the like.

It could also be a drone or something similar.

In the example of the 7a The fighter aircraft includes a quantum computer QC. The quantum computer QC can, for example, in cooperation with a central control unit ZSE of the aircraft FZ, solve the NP-complete problem of risk assessment of objects in the area around the aircraft and along the route to the target, target selection and target definition and the sequence of target engagement, ammunition and weapon selection and work on the fastest and at the same time least risky route to the destination. The quantum computer QC is in the example 7 connected to the central control unit ZSE via an external data bus EXTDB within the aircraft FZ. The quantum computer QC preferably corresponds to a quantum computer QC 1 or the previous description.

In the example of the 7a The exemplary fighter aircraft FZ is armed with a first missile RKT and a second missile RKT. Instead of arming with RKT rockets and/or in addition to arming with rockets, arming with other weapons such as automatic cannons, jammers, reconnaissance devices, etc. is also conceivable. In this respect, the rockets are just examples of additional equipment that can be transported as payload by the FZ fighter aircraft. In this respect, the FZ aircraft is just an example of a vehicle in the broadest sense.

In the example of the 7a The vehicle in the form of the aircraft FZ has a quantum computer system similar to QUSYS 4 with one or more central control devices ZSE, which are connected to one or more quantum computers QC via one or more external data buses EXTDB.

In the example of the 7a The payload in the exemplary form of two RKT rockets each has its own quantum computer systems similar to QUSYS 4 with one or more central control devices ZSE of the respective payload, which are connected via one or more external data buses EXTDB of the respective payload to one or more quantum computers QC of the respective payload. In the example of the 7a Each of the two exemplary rockets RKT has its own quantum computer system QUSYS of the respective rocket RKT similar to 4 with one or more respective central control devices ZSE of the respective rocket RKT, which are connected to one or more quantum computers QC of the respective rocket RKT via one or more external data buses EXTDB of the respective rocket RKT.

In the state shown, the FZ fighter aircraft therefore has several QUSYS quantum computer systems. A first quantum computer system QUSYS includes at least one central control unit ZSE of the fighter aircraft FZ and at least one external data bus EXTDB of the fighter aircraft FZ and at least one quantum computer QC of the fighter aircraft FZ. An exemplary second quantum computer system QUSYS includes at least one central control unit ZSE of the first exemplary rocket RKT and at least one external data bus EXTDB of the first exemplary rocket RKT and at least one quantum computer QC of the first exemplary rocket RKT. An exemplary third quantum computer system QUSYS includes at least one central control unit ZSE of the second exemplary rocket RKT and at least one external data bus EXTDB of the second exemplary rocket RKT and at least one quantum computer QC of the second exemplary rocket RKT.

The document presented here proposes that an external data bus EXTDB connects the first quantum computer system to the second and third quantum computer systems as long as the payloads are connected to the aircraft FZ.

After the rockets RKT have been fired, i.e. when the aircraft FZ separates from its payload in the form of the rockets RKT, a quantum computer system separation device QCTV separates the quantum computer system QUSYS of the separated payload, here the fired rocket RKT, from the quantum computer system QUSYS of the aircraft FZ. The vehicle here is, for example, an aircraft FZ. A vehicle in the sense of the document presented here can also be a motor vehicle, a two-wheeler, a tricycle or a truck, a commercial vehicle, a robot, a transport vehicle, a drone, a robot drone, a missile, a floating body, a submersible body , a ship, a submarine, a sea mine, a landmine, a rocket, a projectile, a satellite, a space station, a trailer, a barge, a container, in particular a sea container or the like. The quantum computer system separation device QCTV preferably separates an external data bus EXTDB, which, for example, connects a first quantum computer system QUSYS with a second quantum computer system QUSYS, if necessary, so that the quantum computer system QUSYS, which previously included the first and the second quantum computer system QUSYS, is separated by the separation using the quantum computer system separation device QCTV in two separate quantum computer systems QUSYS disintegrates. The quantum computer system separating device QCTV can also conversely connect a previously separate first quantum computer system QUSYS with a previously separate second quantum computer system QUSYS, for example via one or more external data buses EXTDB and, if necessary, couple them, so that a new, enlarged quantum computer system QUSYS is created, which then the first and the second Quantum computer system QUSYS comprises merging into a quantum computer system QUSYS by connecting these two quantum computer systems via quantum computer system separation device. In such a new quantum computer system QUSYS made up of at least two previously separate quantum computer systems QUSYS, the central control unit ZSE of the quantum computer system QUSYS of the vehicle, here the fighter aircraft FZ, is preferably given higher priority than the central control unit ZSE of the quantum computer system QUSYS of the payload, here the rocket RKT. This merger is particularly advantageous during the loading process when the payload is connected to the vehicle.

After the payload has been separated from the vehicle, the quantum computer system QUSYS can preferably act autonomously. In the example of the 7a This means that after the separation of the missiles RKT as an exemplary payload from the fighter aircraft FZ as an exemplary vehicle, the quantum computer system QUSYS of the missile RKT can preferably act autonomously. However, it is conceivable that the quantum computer system QUSYS of the payload, here in the form of a rocket RKT, after separation from the vehicle, here in the form of the fighter aircraft FZ, via a wireless or wired or via an optical fiber or a functionally equivalent data transmission link with the quantum computer system QUSYS of the vehicle, here the FZ fighter aircraft, remains connected. In an extreme case, it is conceivable that, for example, each of the quantum computers QC1 to QC16 4 is the quantum computer QC of an individual vehicle, which is connected to a central control unit ZSE in a lead vehicle and/or to each other via a radio link as an external data bus EXTDB. For example, an exemplary quantum computer system QUSYS can be a swarm of drones, in which each of the drones includes one or more quantum computers QC that communicate with each other wirelessly, for example via radio links or laser beam connections as an external data bus EXTDB. In the exemplary case of a swarm of drones, the quantum computer system QUSYS of the quantum computers QC1 to QC16 of the exemplary drones cannot include a central control device ZSE. All drones are preferably designed in approximately the same way and then preferably organize themselves using swarm technologies.

In the example of the 7a For example, each rocket RKT includes a quantum computer QC. The quantum computer QC can, for example, in cooperation with a central control unit ZSE of the relevant missile RKT, solve the NP-complex problem of risk assessment of objects in the vicinity of the relevant missile RKT and along the route of the relevant missile RKT to the target, the target selection and target definition and the sequence of the Target combat by selecting ammunition and weapons and working on the fastest and least risky route to the target. The RKT missile can also be a drone or a cruise missile that can engage multiple targets if necessary. The quantum computer QC of the rocket in question is RKT in the example 7a connected via an external data bus EXTDB within the relevant rocket RKT to the central control unit ZSE of the relevant rocket RKT. The quantum computer QC of the relevant rocket RKT preferably corresponds to a quantum computer QC 1 or the previous description.

Such an FZ aircraft can also, if necessary, exclusively or additionally carry out classic reconnaissance tasks, for example radar remote sensing - especially synthetic aperture radar (SAR). with innovative concepts of quantum technologies. The focus is on more efficient processing of the immense amounts of radar and sensor data from the SENS sensors of the FZ aircraft. Can the quantum hardware presented here, which can also include the aircraft FZ itself, execute quantum algorithms that increase the performance of sensors SENS and/or in particular radar sensors of the aircraft FZ and the processing of the sensor data of the sensors SENS of the aircraft FZ and/or or to accelerate the radar data processing of the radar sensors of the FZ aircraft. Preferably, one or more device components of the aircraft FZ and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to execute one or more quantum algorithms which improve the performance of sensors SENS and/or in particular to increase the radar sensors of the aircraft FZ and/or the radar data processing of the radar sensors of the aircraft FZ and to accelerate the processing of the sensor data of the SENS sensors of the aircraft FZ and/or the radar data processing of the radar sensors of the aircraft FZ.

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. The aircraft FZ and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are preferably set up to solve complex processing and optimization tasks in radar remote sensing and/or exploration of the earth's surface using at least one quantum computer QC using the SENS sensors. Such an application can include, for example, observation and/or analysis of military issues. Preferably one or more device components of the aircraft FZ and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for quantum computing routines and quantum computing methods in the field of radar data processing to carry out. Preferably, one or more device components of the aircraft FZ and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided to focus SAR raw data. Preferably, one or more device components of the aircraft FZ and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and / or intended to carry out SAR interferometry methods. Preferably, one or more device components of the aircraft FZ and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to generate and/or evaluate SAR images.

Figure 7b

The 7b shows an exemplary deployable quantum computer QC in a sea container SC on a low-loader TL with a tractor ZM. Both the sea container SC and the low-loader TL as well as the tractor ZM can include one or more quantum computers QC and/or one or more quantum computer systems QUSYS. One or more quantum computers QC and/or one or more quantum computer systems QUSYS can be placed within the sea container SC. All of these quantum computers QC and/or quantum computer systems QUSYS can be transferred to one or more quantum computer systems QUSYS during transport and/or before and/or afterwards, as in the example 7a explained in particular be interconnected at times. In the example of the 7c An additional energy reserve BENG supplies the quantum computer system QUSYS with the quantum computer QC within the exemplary sea container SC with electrical energy.

Device components of a vehicle (TL, ZM, SC) can also possibly exclusively or additionally combine classic reconnaissance tasks, for example airspace radar monitoring, with innovative concepts of quantum technologies. The focus is on more efficient processing of the immense amounts of radar and sensor data from the vehicle's SENS sensors (TL, ZM, SC). Can the quantum hardware presented here, which can also be part of the vehicle (TL, ZM, SC) itself, execute quantum algorithms that increase the performance of sensors SENS and/or in particular radar sensors of the vehicle (TL, ZM, SC) and to accelerate the processing of the sensor data from the vehicle's SENS sensors (TL, ZM, SC) and/or the radar data processing from the vehicle's radar sensors (TL, ZM, SC). Preferably one or more device components of the vehicle (TL, ZM, SC) and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for this purpose or to execute several quantum algorithms which increase the performance of sensors SENS and/or in particular radar sensors of the vehicle (TL, ZM, SC) and/or the radar data processing of the radar sensors of the vehicle (TL, ZM, SC) and the processing of the sensor data of the sensors To accelerate the vehicle's SENS (TL, ZM, SC) and/or the radar data processing of the vehicle's radar sensors (TL, ZM, SC).

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. The vehicle (TL, ZM, SC) and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are preferably set up to carry out complex processing and optimization tasks in radar remote sensing and/or exploration of the earth's surface using at least one quantum computer QC To release the SENS sensors. Such an application can include, for example, observation and/or analysis of military issues. Preferably one or more device components of the vehicle (TL, ZM, SC) and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for quantum computing routines and quantum computing -To carry out procedures in the area of radar data processing. Preferably one or more device components of the vehicle (TL, ZM, SC) and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for focusing raw sensor data to be carried out. Preferably, one or more device components of the vehicle (TL, ZM, SC) and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to carry out radar interferometry methods. Preferably one or more device components of the vehicle (TL, ZM, SC) and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for recording radar images and/or images Generate and/or evaluate the sensor data from the vehicle's SENS sensors (TL, ZM, SC).

Figure 7c

The 7c shows an exemplary aircraft carrier FZT. The exemplary aircraft carrier FZT includes one or more quantum computers QC and/or one or more quantum computer systems QUSYS. The exemplary aircraft carrier FZT is an example of a warship that includes one or more QC quantum computers and/or one or more QUSYS quantum computer systems. The exemplary aircraft carrier FZT is an example of a ship that includes one or more QC quantum computers and/or one or more QUSYS quantum computer systems. The exemplary aircraft carrier FZT is an example of a floating body that includes one or more quantum computers QC and/or one or more quantum computer systems QUSYS. The exemplary aircraft carrier FZT is an example of a vehicle that includes one or more quantum computers QC and/or one or more quantum computer systems QUSYS. The quantum computers QC and/or quantum computer systems QUSYS are preferably deployable quantum computers QC in the sense of the document presented here. For example, quantum computer systems QUSYS and / or quantum computers QC of aircraft FZ of the aircraft carrier FZT during transport through the aircraft carrier FZT and / or in the aircraft carrier FZT with one or more quantum computers QC and / or quantum computer systems QUSYS of the aircraft carrier FZT, for example via one or more quantum computer system separation devices QCTV and one or more external data buses EXTDB connected to larger quantum computer systems QUSYS.

In the example of the 7c For example, the aircraft carrier FZT includes one or more quantum computers QC and/or one or more quantum computer systems QUSYS. One or more of these quantum computers QC and / or one or more quantum computer systems QUSYS can, for example, in cooperation with a central control unit ZSE of the aircraft carrier FZT, solve the NP-complete problem of risk assessment of objects in the environment of the aircraft carrier FZT and along the route to a target, the target selection and target definition and the sequence of attacking the target, the selection of aircraft, ammunition and weapons and the fastest and at the same time lowest-risk route to the target. The quantum computer(s) QC and/or the quantum computer system(s) QUSYS of the aircraft carrier FZT are preferably connected to each other and to those of other devices via an external data bus EXTDB and, if necessary, suitable quantum computer system separation devices QCTV within the aircraft carrier FZT connected to the aircraft carrier FZT. A quantum computer QC from the aircraft carrier FZT preferably corresponds to a quantum computer QC from the 1 or the previous description.

Device components of the exemplary aircraft carrier FZT can also possibly exclusively or additionally combine classic reconnaissance tasks, for example airspace radar monitoring and/or sonar monitoring of a maritime area, with innovative concepts of quantum technologies. The focus is on the more efficient processing of the immense amounts of radar data and/or sonar data and/or sensor data from the SENS sensors of the exemplary aircraft carrier FZT and the other ships, aircraft, submarines and drones etc. of the association of the exemplary aircraft carrier FZT and the others Data, such as satellite data etc. Can the quantum hardware presented here, which also includes the exemplary aircraft carrier FZT and/or ships, aircraft, submarines and drones etc. of the association of the exemplary aircraft carrier FZT itself, execute quantum algorithms which to increase the performance of sensors SENS and/or in particular radar sensors and/or in particular sonar sensors of the exemplary aircraft carrier FZT or the association of the exemplary aircraft carrier FZT or the other data, such as satellite data, and to process the data and the sensor data of the SENS sensors exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or the radar data processing of the radar sensors of the exemplary aircraft carrier FZT and/or the sonar data processing of the sonar sensors of the exemplary aircraft carrier FZT and the association of the exemplary aircraft carrier FZT are intended to accelerate. Preferably, one or more device components of the exemplary aircraft carrier FZT and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE of the exemplary aircraft carrier FZT are set up and / or intended to execute one or more quantum algorithms, which the performance of sensors SENS and/or in particular radar sensors and/or in particular sonar sensors, in particular of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or the radar data processing of the radar sensors of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or the satellites etc. and/or to increase the sonar data processing of the sonar sensors of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT or a component thereof and to increase the processing of the sensor data of the sensors SENS of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or the radar data processing of the radar sensors of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or the sonar data processing of the sonar sensors of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT or a component thereof .

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. Preferably, the exemplary aircraft carrier FZT and/or parts of the association of the exemplary aircraft carrier FZT and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are set up to carry out complex processing and optimization tasks in radar remote sensing and/or using at least one quantum computer QC Exploration of the earth's surface and/or in sonar exploration and/or exploration of the water surface and/or the airspace and/or the sea area using the SENS sensors. Such an application can include, for example, observation and/or analysis of military issues. Preferably, one or more device components of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for quantum computing. To carry out routines and quantum computing methods in the area of radar data processing and/or sonar data processing. Preferably, one or more device components of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for focusing of raw sensor data. Preferably, one or more device components of the exemplary aircraft carrier FZT and / or the association of the exemplary aircraft carrier FZT and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and / or provided for this purpose, method of To carry out radar interferometry and/or sonar interferometry. Preferably So one or more device components of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to produce radar images and/or or to generate and/or evaluate sonar images and/or images based on the sensor data of the SENS sensors of the exemplary aircraft carrier FZT and/or the association of the exemplary aircraft carrier FZT and/or satellite data and/or other data.

Figure 7d

The 7d shows a factory hall FHB as an example of a stationary device into which several QC quantum computers were installed. In the example of the 7d The normal power network PWR supplies the deployable quantum computer systems QUSYS with their quantum computers QC within the exemplary stationary devices FBH with electrical energy. The stationary device FHB can, for example, comprise one or more quantum computer systems QUSYS with one or more quantum computers QC. The quantum computer(s) QC and/or the quantum computer system(s) QUSYS of the stationary device FHB are preferably connected to each other and to those of other devices of the stationary device FHB via an external data bus EXTDB and possibly suitable quantum computer system separation devices QCTV within the stationary device FHB. A quantum computer QC of the stationary device FHB preferably corresponds to a quantum computer QC of 1 or the previous description.

Figure 8

8th shows another example of a vehicle with a proposed quantum computer system QUSYS, here with two quantum computers QC as an example. It is an exemplary submarine SUB. The exemplary submarine SUB has an energy system ERS as the energy source of the submarine SUB. The energy system ERS also represents the energy supply PWR of the charging device LDV of the quantum computer system QUSYS of the submarine SUB. The submarine SUB typically has a very large energy reserve BTR. A drive ENG drives in the example 8th the submarine SUB via one or more exemplary ship screws SCHR.

In the example of the 8th The submarine SUB has a number of RKT missiles as armament. They can also be cruise missiles or other devices that are located on the submarine SUB as devices that can be separated from the submarine SUB. In this respect, the RKT rockets are only examples of devices that can be separated from a vehicle and, for example, as a payload here, are located on or in the vehicle, here a submarine SUB. For example, one or more of the missiles RKT of the submarine SUB may include one or more quantum computer systems QUSYS and/or one or more quantum computers QC. Preferably, the one or more quantum computer systems QUSYS and/or one or more quantum computers QC are connected to the one or more quantum computer systems QUSYS and/or the one or more quantum computers QC1, QC2 of the submarine SUB by means of a quantum computer system separation device QCTV and an external data bus EXTDB tied together. The document presented here already describes the separation and connection of quantum computer systems QUSYS in the description 7a . Here the submarine SUB takes on the role of the aircraft FZ 7a a. The relationships disclosed there also apply here where applicable and are used where appropriate and sensible. A missile launch control RKTC is an example of a vehicle fire control system. Here the vehicle is the submarine SUB. In the example of the 8th The missile launch control RKTC and the submarine SUB can each have one or more quantum computer systems QUSYS and / or one or more quantum computers QC. Since the missile launch control RKTC is part of the submarine, the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the missile launch control RKTC are also part of the submarine SUB. An external data bus EXTDB preferably connects the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the missile launch control RKTC with the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the submarine SUB.

In the example of the 8th The submarine SUB has a number of TRP torpedoes as armament. They can be cruise missiles or other devices that are located on the submarine SUB as devices that can be separated from the submarine SUB and are separated, for example, via the torpedo tubes as an example of a mechanical separation device, for example by firing. In this respect, the TRP torpedoes are just examples of devices that can be separated from a vehicle and, for example, like this as payload is on or in the vehicle, here a submarine SUB. For example, one or more of the torpedoes TRP of the submarine SUB may include one or more quantum computer systems QUSYS and/or one or more quantum computers QC. The one or more quantum computer systems QUSYS and/or one or more quantum computers QC are preferred by means of a quantum computer system separation device QCTV and an external data bus EXTDB with the one and/or more quantum computer systems QUSYS and/or the one or more quantum computers QC1, QC2 of the submarine SUB tied together. The document presented here already describes the separation and connection of quantum computer systems QUSYS in the description 7a . Here the submarine SUB takes on the role of the aircraft FZ 7a a. The connections disclosed there also apply here where applicable and are used where appropriate and meaningful. A torpedo launch control TRPC is an example of a vehicle's fire control system. Here the vehicle is the submarine SUB. In the example of the 8th The torpedo launch control TRPC and the submarine SUB can each have one or more quantum computer systems QUSYS and / or one or more quantum computers QC. Since the torpedo launch control TRPC is part of the submarine SUB, the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the torpedo launch control RKTC are also part of the submarine SUB. An external data bus EXTDB preferably connects the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the torpedo launch control TRPC with the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the submarine SUB.

In addition, the submarine SUB in the example has the 8th preferably via a large number of sensors SENS, which, for example, connects an external data bus EXTDB with one or more quantum computer systems QUSYS and / or quantum computers QC on board the submarine SUB. These can be, for example, sound sensors and/or ultrasonic sensors, conductivity sensors, antennas, sensors for electromagnetic and/or ionizing radiation, particle detectors, pressure sensors, speed sensors, position sensors, attitude sensors, acceleration sensors, magnetometers, LIDAR sensors, RADAR sensors, quantum sensors and the like act equally. The SENS sensors can also be sensor systems, sensor arrays and other measuring systems. The SENS sensors can record measured values inside and outside the vehicle, here a submarine SUB. Preferably one or more of the quantum computers QC1, QC2 evaluates the sensor data from the SENS sensors. Typically, at least temporarily, states of one or more quantum dots (NV1, NV2) of one or more quantum computers of the quantum computers QC1, QC2 depend directly or indirectly on the values of the sensor data from the SENS sensors, in particular after processing by the computer core CPU or another data processing system.

In the example of the 8th For example, one or more quantum computers QC and / or one or more quantum computer systems QUSYS on board the vehicle, here a submarine SUB, for example in cooperation with a central control unit ZSE of the vehicle, the NP-complete problem of risk assessment of objects in the area around the vehicle, here for example the submarine SUB, and/or along the course to the target of the vehicle, the target selection and target definition and the sequence of target engagement, the ammunition and weapon selection and the fastest and at the same time lowest-risk route of the vehicle to the target. In this case, one or more of the quantum computers QC1, QC2 preferably evaluate the sensor data of the sensors SENS and preferably change at least temporarily the states of one or more quantum dots (NV1, NV2) of one or more quantum computers of the quantum computers QC1, QC2 depending on the values of the sensor data of the Sensors SENS in a direct or indirect manner, especially after processing by the computer core CPU or another data processing system.

The quantum computers QC1, QC2 of the submarine SUB and the other device parts are in the example 8th connected to the central control unit ZSE of the submarine SUB via an external data bus EXTDB within the submarine SUB. The quantum computers QC1, QC2 and those of the other device parts preferably correspond to a quantum computer QC 1 or the previous description.

Device components of the submarine SUB can also, if necessary, exclusively or additionally combine classic reconnaissance tasks, for example airspace radar monitoring and/or sonar monitoring of a marine area, with innovative concepts of quantum technologies. The focus is on more efficient processing of the immense amounts of radar data and/or sonar data and/or sensor data from the SENS sensors of the submarine SUB and the other ships, aircraft, submarines and drones, etc. of the association of the submarine SUB and other data, such as satellite data etc.. Can the quantum hardware presented here, which can also include the submarine SUB and/or ships, aircraft, submarines and drones etc. of the submarine SUB itself, execute quantum algorithms , which increase the performance of sensors SENS and/or in particular radar sensors and/or in particular sonar sensors of the submarine SUB or the association of the submarine SUB or the other data, such as satellite data, and the processing of the data and the sensor data of the SENS sensors Submarine SUB and / or the association of the submarine SUB and / or the radar data processing of the radar sensors of the submarine SUB and / or the sonar data processing of the sonar sensors of the submarine SUB and the association of the submarine SUB should accelerate. Preferably, one or more device components of the submarine SUB and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE of the submarine SUB are set up and/or intended to execute one or more quantum algorithms which improve the performance of sensors SENS and/or in particular radar sensors and/or in particular sonar sensors, in particular of the submarine SUB and/or the association of the submarine SUB and/or the radar data processing of the radar sensors of the submarine SUB and/or the association of the submarine SUB and/or the satellites etc .and/or to increase the sonar data processing of the sonar sensors of the submarine SUB and/or the association of the submarine SUB or a component thereof and the processing of the sensor data of the sensors SENS of the submarine SUB and/or the association of the submarine SUB and/or the radar data processing of the To accelerate radar sensors of the submarine SUB and/or the association of the submarine SUB and/or the sonar data processing of the sonar sensors of the submarine SUB and/or the association of the submarine SUB or a component thereof.

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. Preferably, the submarine SUB and/or parts of the association of the submarine SUB and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are set up to carry out complex processing and optimization tasks in radar remote sensing and/or exploration using at least one quantum computer QC Earth's surface and/or in sonar exploration and/or exploration of the water surface and/or the airspace and/or the sea area using the SENS sensors. Such an application can include, for example, observation and/or analysis of military issues. Preferably, one or more device components of the submarine SUB and / or the association of the submarine SUB and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and / or provided for quantum computing routines and - To carry out quantum computing methods in the area of radar data processing and/or sonar data processing. Preferably, one or more device components of the submarine SUB and / or the association of the submarine SUB and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and / or provided for focusing the sensor -make raw data. Preferably, one or more device components of the submarine SUB and / or the association of the submarine SUB and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and / or provided for this purpose, methods of radar interferometry and /or carry out sonar interferometry. Preferably, one or more device components of the submarine SUB and / or the association of the submarine SUB and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and / or provided for radar images and / or To generate and/or evaluate sonar images and/or images based on the sensor data of the SENS sensors of the submarine SUB and/or the association of the submarine SUB and/or satellite data and/or other data.

Figure 9

9 shows an exemplary vehicle with a first quantum computer QC1, a second quantum computer QC2, a central control unit ZSE and an external data bus EXTDB, which connects them to a quantum computer system QUSYS. The vehicle in the example is the 9 an exemplary motor vehicle. As exemplary sensors SENS, the vehicle includes a GPS receiver GPS for determining the current position on the earth's surface and a navigation system NAV. The vehicle can have one or more quantum computers QC and/or a or include multiple quantum computer systems QUSYS, which can be connected to one another via one or more external data buses EXTDB. The one or more external data buses can connect the one or more quantum computers QC and/or one or more quantum computer systems QUSYS with one or more actuators and/or one or more sensors. The SENS sensors can also be sensor systems. For example, these can be acceleration and position sensors, impact sensors, ultrasonic measurement systems, radar systems, LIDAR systems, drive sensor systems and energy storage systems, etc. The actuators can be transmitters, lasers, motors, etc. In this case, one or more of the quantum computers QC1, QC2 preferably evaluate the sensor data of the sensors SENS and preferably change at least temporarily the states of one or more quantum dots (NV1, NV2) of one or more quantum computers of the quantum computers QC1, QC2 depending on the values of the sensor data of the Sensors SENS in a direct or indirect manner, especially after processing by the computer core CPU or another data processing system.

In the example of the 9 For example, one or more quantum computers QC and / or one or more quantum computer systems QUSYS on board the vehicle, here a car, for example in cooperation with a central control unit ZSE of the vehicle, the NP-complete problem of risk assessment of objects in the area around the vehicle, here for example the car, and/or along the route to the vehicle's destination, the destination selection and destination definition and the order of approach to the destination and the fastest and at the same time lowest-risk route of the vehicle to the destination. The quantum computers QC1, QC2 of the vehicle, here an example of the car, and the other device parts of the vehicle, here an example of the car, are in the example 9 via an external data bus EXTDB within the vehicle, here for example the car, preferably connected to the central control unit ZSE of the vehicle, here for example the car. The quantum computers QC1, QC2 and those of the other device parts preferably correspond to a quantum computer QC 1 or the previous description.

Device components of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, can also possibly exclusively or additionally combine classic reconnaissance tasks, for example airspace radar monitoring, with innovative concepts of quantum technologies. The focus here is on the more efficient processing of the immense amounts of radar data and/or ultrasound data and/or sensor data from the SENS sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and the other data, such as satellite data etc. Can the quantum hardware presented here, whose part can also be the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car itself, execute quantum algorithms that improve the performance of sensors SENS and/or in particular radar sensors and/or in particular ultrasonic sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, or the other data, such as satellite data, and the processing of the data and the sensor data of the SENS sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and / or the radar data processing of the radar sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and/or the ultrasound data processing of the ultrasonic sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car. Preferably one or more device components of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, are set up and / or intended to execute one or more quantum algorithms, which the performance of sensors SENS and / or in particular radar sensors and / or in particular Ultrasonic sensors, in particular d of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and / or the radar data processing of the radar sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and/or the ultrasonic sensor data of the ultrasonic sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and/or the satellites etc. or a component thereof and the processing the sensor data of the SENS sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and/or the radar data processing of the radar sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and/or the sonar data processing of the sonar sensors of the vehicle, here for example the car, and the other device parts of the Vehicle, here for example the car, or a component thereof.

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. Preferably, the vehicle, here by way of example the car, and the other device parts of the vehicle, here by way of example the car, and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are set up to carry out complex processing using at least one QC quantum computer. and to solve optimization tasks in radar exploration and/or in ultrasonic exploration and/or the airspace using the SENS sensors. Such an application can include, for example, observation and/or analysis of military issues. Preferably one or more device components of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE set up and/or intended to carry out quantum computing routines and quantum computing methods in the area of radar data processing and/or ultrasound data processing. Preferably one or more device components of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE set up and/or intended to focus sensor raw data. Preferably one or more device components of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE set up and/or intended to carry out methods of radar interferometry and/or ultrasonic interferometry. Preferably one or more device components of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and / or the quantum computer system QUSYS and / or the quantum computers QC1, QC2 and possibly the central control unit ZSE set up and/or intended for this purpose, radar images and/or ultrasound images and/or images based on the sensor data of the SENS sensors of the vehicle, here for example the car, and the other device parts of the vehicle, here for example the car, and/or satellite data and/or other data to be generated and/or evaluated.

Figure 10

10 shows a typical solution to an NP-complete problem. The development of the proposal presented here showed that problem solving with a quantum computer takes place in four instead of three steps.

Computer programs that run on conventional computers with Harvard or non-Neumann architecture prefer to solve problems using the steps of analysis, elaboration and synthesis.

In the analysis step (step A)), the computer adapts the problem to the way the computer works. For example, a read routine translates a text file with readable numbers into binary data that is stored in the computer's memory.

In a second step, elaboration (step B), the computer then carries out a calculation in which, for example, these binary data serve as input data and determines binary result data.

In a third step, the synthesis step (step D), the computer adapts this result to the intended use. For example, in the example described here, the computer could convert the binary result data into readable digits of the corresponding numbers in an output text file.

The elaboration has now shown that, particularly in safety-relevant applications, after a solution to an NP-complete problem in elaboration step B) using a quantum computer QC, the quantum computer system QUSYS must carry out a check in step C). In this test step, the quantum computer system QUSYS or the quantum computer QC checked, preferably using a conventional computer core CPU or a central control unit ZSE, whether the solution determined in the elaboration is actually a solution. In quantum operations These are always statistical operations that can also produce incorrect results. If necessary, the QUSYS quantum computer system repeats the calculation.

Figure 11

11 equals to 4 , whereby the 16 quantum computers QC1 to QC16 of the quantum computer system QUSYS are now inserted into the external data bus EXTDB as an example. The control device μC, for example, of each of the quantum computers QC1 to QC16, has, for example, two external data interfaces DBIFa and DBIFb instead of a data bus interface DBIF, as in 1 shown. This allows, for example, the central control unit ZSE to assign each of the quantum computers QC a unique bus node address. Typically, the control devices µC of the quantum computers QC1 to QC16 pass on data that they pass on from the data bus side with the central control device ZSE to quantum computers and bus nodes on the other half of the data bus only if they themselves have already received a valid bus node address from the central control device ZSE. In this way, the central control device ZSE can gradually assign a quantum computer address as a bus node address of the external data bus EXTDB to all quantum computers of the quantum computers QC1 to QC16, starting with the first quantum computer QC1. After switching on or a system reset, all quantum computers QC1 to QC16 preferably have an invalid default quantum computer address that is typically the same as the initial bus node address. As a result, the central control device can provide the quantum computer QC1 to QC16 that is not yet provided with a valid bus node address and is closest to it with a valid bus node address. As a result, in the next step, the central control device ZSE can reach and initialize the underlying quantum computer of the quantum computers QC1 to QC16 and so on until all quantum computers of the quantum computers QC1 to QC16 have received a valid quantum computer address as a bus node address. After switching on, the quantum computer system QSYS preferably carries out an initialization of the quantum computers QC1 to QC16 of the quantum computer system QUSYS. The initialization of the QUSYS quantum computer system preferably also includes carrying out an auto-addressing process for assigning bus node addresses to the bus nodes of the external data bus EXTDB. In the example of the 11 The bus nodes are the quantum computers QC1 to QC16. In the example of the 11 The central control device ZSE preferably takes on the role of a bus master, which generates and assigns the bus node addresses and controls the quantum computers QC1 to QC16.

Figure 12

12 shows an exemplary quantum computer system QUSYS with four sub-quantum computer systems.

The first quantum computer QC1 forms a first sub-quantum computer system with the second quantum computer QC2 and the third quantum computer QC3 and the fourth quantum computer QC4. A first sub-data bus UDB1 connects the quantum computers QC1, QC2, QC3, QC4 of the first sub-quantum computer system. The first quantum computer QC1 can serve as a bus master for the other quantum computers QC2, QC3, QC4 of the first sub-quantum computer system.

The fifth quantum computer QC5 forms a second sub-quantum computer system with the sixth quantum computer QC6 and the seventh quantum computer QC7 and the eighth quantum computer QC8. A second sub-data bus UDB2 connects the quantum computers QC5, QC6, QC7, QC8 of the second sub-quantum computer system. The fifth quantum computer QC5 can serve as a bus master for the other quantum computers QC6, QC7, QC8 of the second sub-quantum computer system.

The ninth quantum computer QC9 forms a third sub-quantum computer system with the tenth quantum computer QC10 and the eleventh quantum computer QC11 and the twelfth quantum computer QC12. A third sub-data bus UDB3 connects the quantum computers QC9, QC10, QC11, QC12 of the third sub-quantum computer system. The ninth quantum computer QC9 can serve as a bus master for the other quantum computers QC10, QC11, QC12 of the third sub-quantum computer system.

The thirteenth quantum computer QC13 forms a fourth sub-quantum computer system with the fourteenth quantum computer QC14 and the fifteenth quantum computer QC15 and the sixteenth quantum computer QC16. A fourth sub-data bus UDB4 connects the quantum computers QC13, QC14, QC15, QC16 of the fourth sub-quantum computer system. The thirteenth quantum computer QC13 can serve as a bus master for the other quantum computers QC14, QC15, QC16 of the fourth sub-quantum computer system.

In the example of the 12 the external data bus EXTDB connects the first quantum computer QC1 and the fifth quantum computer QC5 and the ninth quantum computer QC9 and the thirteenth quantum computer QC13 and the central control unit ZSE.

Figure 13

13 shows the solution of an NP-complete problem using a mobile deployable quantum computer QC. Such a method begins with the acquisition of environmental data by the QUSYS quantum computer system in step A). The environmental data is typically collected using suitable sensors, which can be part of the quantum computer system QUSYS or which are connected to this quantum computer system QUSYS via data connections and transmit environmental data to the quantum computer system QUSYS. In a step B), the quantum computer system QUSYS identifies objects in the environment of the quantum computer system QUSYS, whereby this environment can also be distant from the quantum computer system QUSYS. In step C), the quantum computer system QUSYS classifies the identified objects in the environment of the quantum computer system QUSYS. Typically, in step C), the quantum computer system QUSYS classifies the objects according to danger and/or vulnerability and/or strategic effect in order to maximize a weapon effect. This classification is preferably carried out in step C) using a neural network model, which the quantum computer system QUSYS preferably executes. For this step C), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out the classification of the objects. In a step D, the quantum computer system QUSYS determines the weapons and/or the ammunition and/or the configuration and/or the order of the attacked objects and/or the attacked and/or the non-attacked objects. This determination is preferably carried out in step D) using a neural network model, which the quantum computer system QUSYS preferably executes. In step D), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out these determinations. In a step E), the quantum computer system QUSYS preferably suggests one or more of these specified attack scenarios to an operator, for example one or more pilots and/or several fire control officers or the like. If they give the order to fire, the quantum computer system QUSYS, for example, can implement the released attack scenario in a step F).

This example application can be generalized to solve NP-complete problems. Such a generalized method begins with the acquisition of data by the quantum computer system QUSYS in a step A). The data is typically collected using suitable sensors and/or databases or other data sources, which can be part of the quantum computer system QUSYS or which are connected to this quantum computer system QUSYS via data connections and transmit the data to the quantum computer system QUSYS. In a step B), the quantum computer system QUSYS identifies suitable data objects. In step C), the QUSYS quantum computer system classifies the identified data objects. Typically, in step C), the quantum computer system QUSYS classifies the objects according to categories that are relevant to solving the respective problem in order to maximize the effect. This classification is preferably carried out in step C) using a neural network model, which the quantum computer system QUSYS preferably executes. For this step C), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum points NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out the classification of the data objects. In a step D), the quantum computer system QUSYS determines the means for achieving the purpose and the parameters and means configurations when using these means and/or the order of the processed or unprocessed data objects and/or the order of the means used. This determination is preferably carried out in step D) using a neural network model, which the quantum computer system QUSYS preferably executes. The quantum computer system QUSYS preferably uses one or more quantum operations in step D) to manipulate the quantum state of one or more quantum points NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out these determinations. In a step E), the quantum computer system QUSYS preferably suggests one or more of these specified scenarios to an operator or the like. If they give a start signal, the QUSYS quantum computer system can, for example, implement the released scenario in a step F).

Figure 14

The 14 shows an exemplary structure of an amplifier V, as shown in the 1 is marked. An internal amplifier IVV of the amplifier V amplifies and filters the receiver output signal S0 to an output signal V1 of the internal amplifier IVV of the amplifier V. An analog-to-digital converter ADCV of the amplifier V converts the output signal V1 of the internal amplifier IVV of the amplifier V to digitized ones Sample values on a data line V2 between the control device µCV of the amplifier V and the analog-to-digital converter ADCV of the amplifier V. The control device µCV of the amplifier V and preferably stores these sample values in a memory MEMV of the amplifier V; via a memory data bus MEMDBV between the control device µCV of the amplifier V and the memory MEMV of the amplifier V. The control device µC of the deployable quantum computer QC can then access the data in the memory MEMV of the amplifier V via the control data bus SDB, the data interface VIF of the amplifier V, the internal control data bus SDBV of the amplifier V and the control device µCV of the amplifier V and further process it.

Figure 15

15 shows an example of a garment with a deployable quantum computer system QUSYS. For rework, the document presented here refers to the document as an example WO 2020 239 172 A1 , which reveals a method for CMOS integration.

The document presented here proposes incorporating one or more quantum computers QC1, QC2 and a central control unit ZSE into the material of a garment KLST. The quantum computer system QUSYS preferably corresponds to the quantum computer system QUSYS 4 , 11 or 12 or similar. The item of clothing can also be a wristwatch or the like.

Device components of clothing KLST can also, if necessary, exclusively or additionally combine classic monitoring tasks, for example environmental monitoring, with innovative concepts of quantum technologies. The focus is on more efficient processing of the immense amounts of sensor data from the SENS sensors of the KLST garment and other data. The quantum hardware presented here, which can also be part of the KLST garment itself, can execute quantum algorithms that increase the performance of the SENS sensors of the KLST garment or the other data and the processing of the data and the sensor data of the SENS sensors of the garment KLST should accelerate. Preferably, one or more device components of the garment KLST and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE of the garment KLST are set up and/or provided to execute one or more quantum algorithms which improve the performance of To increase the SENS sensors of the garment KLST and to accelerate the processing of the sensor data of the SENS sensors of the garment KLST.

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. The garment KLST and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are preferably set up to solve complex processing and optimization tasks using the SENS sensors using at least one quantum computer QC. Such an application can include, for example, observation and/or analysis of military issues. Preferably, one or more device components of the garment KLST and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to carry out quantum computing routines and quantum computing methods in the area of environmental data processing .

Figure 16

16 shows an example of a satellite or spacecraft as an example of a vehicle with a deployable quantum computer system QUSYS. The document presented here proposes integrating one or more quantum computers QC1, QC2 and a central control unit ZSE into the satellite or spacecraft. The quantum computer system QUSYS preferably corresponds to the quantum computer system QUSYS 4 , 11 or 12 or similar.

• • von Sensoren SENS und/oder
• • insbesondere von Radarsensoren des Satelliten bzw. des Raumfahrzeugs und/oder
• • insbesondere von LIDAR-Sensoren des Satelliten bzw. des Raumfahrzeugs und/oder
• • die Radardatenverarbeitung der Daten der Radarsensoren des Satelliten bzw. des Raumfahrzeugs und/oder
• • die LIDAR-Datenverarbeitung der Daten der LIDAR-Sensoren des Satelliten bzw. des Raumfahrzeugs

zu steigern und/oder die Verarbeitung der Sensordaten der Sensoren SENS des Satelliten bzw. des Raumfahrzeugs und/oder die Radardatenverarbeitung der Radarsensoren des Satelliten bzw. des Raumfahrzeugs und/oder die LIDAR-Datenverarbeitung der Radarsensoren des Satelliten bzw. des Raumfahrzeugs beschleunigen.Such a satellite or spacecraft can combine classic reconnaissance tasks of radar remote sensing - especially synthetic aperture radar (SAR) - and/or LIDAR exploration (LIDAR = Light imaging, detection and ranging) with innovative concepts of quantum technologies . In the The focus is on more efficient processing of the immense amounts of radar and/or LIDAR data. Can the quantum hardware presented here, which can be part of the satellite or the spacecraft itself, execute quantum algorithms that increase the performance of SENS sensors and/or in particular radar sensors and/or LIDAR sensors and the processing of the sensor data of the SENS sensors Satellites or the spacecraft and / or the radar data processing of the radar sensors of the satellite or the spacecraft and / or the LIDAR data processing of the LIDAR sensors of the satellite or the spacecraft are intended to accelerate. Preferably, one or more device components of the satellite or spacecraft and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided to execute one or more quantum algorithms which improve the performance

• • from sensors SENS and/or
• • in particular from radar sensors of the satellite or spacecraft and/or
• • in particular from LIDAR sensors of the satellite or spacecraft and/or
• • the radar data processing of the data from the radar sensors of the satellite or spacecraft and/or
• • LIDAR data processing of the data from the LIDAR sensors of the satellite or spacecraft

to increase and/or accelerate the processing of the sensor data of the SENS sensors of the satellite or spacecraft and/or the radar data processing of the radar sensors of the satellite or spacecraft and/or the LIDAR data processing of the radar sensors of the satellite or spacecraft.

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. The satellite or the spacecraft and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are preferably set up to use at least one quantum computer QC to solve complex processing and optimization tasks in radar remote sensing and/or the exploration of the planetary surface using the SENS sensors . Previous space-based radar and/or LIDAR sensors were able to image the Earth's surface twice a year. Due to the higher processing speed, such a satellite or spacecraft can deliver pre-processed and pre-analyzed sensor data from the SENS sensors of the entire earth's surface up to twice a week by the quantum computer system QUSYS instead of twice a year. Preferably, one or more device components of the satellite or spacecraft and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to implement quantum computing routines and quantum computing methods To carry out the area of radar data processing and/or LIDAR data processing. Preferably, one or more device components of the satellite or spacecraft and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided to focus SAR raw data. Preferably, one or more device components of the satellite or spacecraft and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to carry out SAR interferometry methods. Preferably, one or more device components of the satellite or spacecraft and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for using one or the quantum computer system QUSYS SAR- Generate and/or evaluate images and/or radar images and/or LIDAR images.

Figure 17

17 shows an example of a smartphone with a deployable QUSYS quantum computer system. The document presented here proposes integrating one or more quantum computers QC1, QC2 and a central control unit ZSE into the smartphone. For rework, the document presented here refers to the document as an example WO 2020 239 172 A1 , which reveals a method for CMOS integration. The quantum computer system QUSYS preferably corresponds to the quantum computer system QUSYS 4 , 11 or 12 or similar.

Device components of the smartphone can also combine exclusively or additionally classic monitoring tasks, for example environmental monitoring, with innovative concepts of quantum technologies. In the foreground This involves more efficient processing of the immense amounts of sensor data from the smartphone's SENS sensors and other data. Can the quantum hardware presented here, which can also be part of the smartphone itself, execute quantum algorithms that are intended to increase the performance of the smartphone's SENS sensors or other data and accelerate the processing of the data and the sensor data of the smartphone's SENS sensors . Preferably, one or more device components of the smartphone and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE of the smartphone are set up and/or intended to execute one or more quantum algorithms which determine the performance of sensors To increase the SENS of the smartphone and to accelerate the processing of the sensor data from the SENS sensors of the smartphone.

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. The smartphone and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are preferably set up to solve complex processing and optimization tasks using the SENS sensors using at least one quantum computer QC. Such an application can include, for example, observation and/or analysis of military issues. Preferably, one or more device components of the smartphone and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to execute quantum computing routines and quantum computing methods in the area of environmental data processing .

Figure 18

18 shows an exemplary drone swarm with a first drone DR1 and a second drone DR2 and a third drone DR3. The drones are examples of unmanned aerial vehicles. The principle can also be transferred to swarms of unmanned floating bodies and unmanned robots (land vehicles). Mixtures of these are also conceivable.

18 shows another example of the use of the proposed deployable quantum computer QC in the drones DR1, DR2, DR3 of a drone swarm. In the example of the 18 The drones DR1, DR2, DR3 are exemplary quadrocopters.

In the example of the 18 Each drone of the example includes a first quantum computer QC1 and a second quantum computer QC2. The quantum computers QC1, QC2 can, for example, in cooperation with a central control unit ZSE of the respective drone of the drones DR1, DR2, DR3 FZ, solve the NP-complete problem of risk assessment of objects in the area around the aircraft and along the route to the target, target selection and target setting and the order of attacking the target, the selection of ammunition and weapons and the fastest and at the same time least risky route to the target and the appropriate formation of the drone swarm on the way there. The quantum computers QC1, QC2 are in the example 18 via an external data bus EXTDB within the respective drone of the DR1, DR2, DR3 with the central control unit ZSE within the respective drone of the DR1, DR2, DR3. In the example of the 18 For example, the central control unit ZSE is inserted into the external data bus EXTDB. The networks of the drones DR1, DR2, DR3 are preferably connected to one another by means of wireless connections, so that the quantum computers of the drones DR1, DR2, DR3 form a common quantum computer system QUSYS with the central control units ZSE of the drones DR1, DR2, DR3. The quantum computers QC1, QC2 of the drones DR1, DR2, DR3 each preferably correspond to a quantum computer QC 1 or the previous description.

In the example of the 18 The drones DR1, DR2, DR3 are each equipped with a camera as a payload. Instead of such a payload, arming with RKT rockets and/or arming with other weapons such as automatic cannons, jammers, reconnaissance devices, etc. is also conceivable. In this respect, the cameras are just examples of additional equipment that can be transported as payload by the drones DR1, DR2, DR3. In this respect, the drones DR1, DR2, DR3 are just an example of a quantum computer-controlled swarm in the broadest sense.

In the example of the 18 The DR1, DR2, DR3 drones have a quantum computer system similar to QUSYS 4 with one or more central control devices ZSE, which are connected to one or more quantum computers QC1, QC2 via one or more external data buses EXTDB.

In the state shown, the drone swarm therefore has several QUSYS quantum computer systems in the respective drones DR1, DR2, DR3.

A first quantum computer system QUSYS of a first drone DR1 comprises at least one central control unit ZSE of the first drone DR1 and at least one external data bus EXTDB of the first drone DR1 and at least a first quantum computer QC1 of the first drone DR1 and in the example a second quantum computer QC2 of the first drone DR1.

A second quantum computer system QUSYS of a second drone DR2 comprises at least one central control unit ZSE of the second drone DR2 and at least one external data bus EXTDB of the second drone DR2 and at least a first quantum computer QC1 of the second drone DR2 and in the example a second quantum computer QC2 of the second drone DR2.

A third quantum computer system QUSYS of a third drone DR3 comprises at least one central control unit ZSE of the third drone DR3 and at least one external data bus EXTDB of the third drone DR3 and at least a first quantum computer QC1 of the third drone DR3 and in the example a second quantum computer QC2 of the third drone DR3.

The document presented here suggests that a radio connection connects the three external data buses EXTDB of the three drones DR1, DR2, DR3 and thus the first quantum computer system with the second and third quantum computer systems.

The 18 thus discloses a swarm of vehicles with swarm members - here the drones DR1, DR2, DR3 -, with at least some of the swarm members each comprising at least one quantum computer QC1, as described above.

Preferably, at least some of the swarm members each comprise at least one such quantum computer QC1 in a quantum computer system QUSYS and at least one further such quantum computer QC2 and/or at least one central control unit ZSE in the form of a conventional computer system.

The QUSYS quantum computer systems of at least two swarm members, better of several swarm members, even better of all swarm members are preferably coupled to one another by means of a wireless data transmission link. Within the meaning of this document, wireless transmission links can be acoustic and/or optical and/or electromagnetic and/or particle-based or the like. This has the advantage that the drone swarm can reconfigure itself even if a single drone fails.

A swarm member within the meaning of the document presented here can also be a vehicle, a motor vehicle, a two-wheeler, a tricycle or a truck, a commercial vehicle, a robot, a transport vehicle, a drone, a robot drone, a missile, a floating body , a diving body, a ship, a submarine, a sea mine, a landmine, a rocket, a projectile, a satellite, a space station, a trailer, a barge, a container, in particular a sea container and / or smartphone and/or a garment and/or a piece of jewelry and/or a wearable quantum computer system and/or a mobile quantum computer system and/or vehicle and/or robot and/or aircraft and/or a rum missile and/or underwater vehicle and/or surface floating body and/or Underwater floating body and/or a movable medical device and/or a deployable weapon system and/or warhead and/or surface or underwater vehicle and/or projectile and/or other mobile device and/or movable device and/or the like.

Device components of the drone swarm can also, if necessary, exclusively or additionally combine classic reconnaissance tasks, for example airspace radar monitoring and environmental monitoring, with innovative concepts of quantum technologies. The focus is on the more efficient processing of the immense amounts of radar data and/or LIDAR data and/or ultrasound data and/or sensor data from the SENS sensors of the drones DR1, DR2, DR3 of the drone swarm and other data, such as satellite data, etc. This can be done here presented quantum hardware, part of which can also be the drones DR1, DR2, DR3 of the drone swarm and the drone swarm itself, execute quantum algorithms which increase the performance of sensors SENS and/or in particular radar sensors and/or LIDAR sensors and/or in particular ultrasonic sensors of the Drones DR1, DR2, DR3 of the drone swarm or other data, such as satellite data, and the processing of the data and the sensor data of the SENS sensors of the drones DR1, DR2, DR3 of the drone swarm and / or the radar data processing of the radar sensors of the drones DR1, DR2, DR3 of the drone swarm and/or the LIDAR data of the drones DR1, DR2, DR3 of the drone swarm and/or the ultrasonic data processing of the Ultra data sound sensors of the drones DR1, DR2, DR3 of the drone swarm should accelerate. Preferably one or more device components of one or more drones DR1, DR2, DR3 of the drone swarm and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE of one or more drones DR1, DR2, DR3 of the drone swarm set up and/or intended to execute one or more quantum algorithms which determine the performance of sensors SENS and/or in particular radar sensors and/or LIDAR sensors and/or in particular ultrasonic sensors, in particular the drones DR1, DR2, DR3 of the drone swarm and/or the Radar data processing of the data from the radar sensors of the drones DR1, DR2, DR3 of the drone swarm and/or the satellites etc. and/or the LIDAR data processing of the data from the LIDAR sensors of the drones DR1, DR2, DR3 of the drone swarm and/or the ultrasonic data processing of the data of the ultrasonic sensors of the drones DR1, DR2, DR3 of the drone swarm or a component thereof and the processing of the sensor data of the SENS sensors of the drones DR1, DR2, DR3 of the drone swarm and/or the radar data processing of the data of the radar sensors of the drones DR1, DR2, DR3 of the drone swarm and/or the LIDAR data processing of the data from the LIDAR sensors of the drones DR1, DR2, DR3 of the drone swarm and/or the sonar data processing of the data from the sonar sensors of the drones DR1, DR2, DR3 of the drone swarm or a component thereof.

One or more of the sensors are preferably SENS quantum sensors. Quantum sensors in the sense of the document presented here are sensors that use at least one quantum dot (NV1, NV2) to determine a measured value for a physical quantity and to transmit this measured value to the quantum computer system (QUSYS, ZSE, QC1, QC2) and/or a quantum computer QC to provide. Preferably, one or more drones DR1, DR2, DR3 of the drone swarm and/or the quantum computer system (QUSYS, ZSE, QC1, QC2) are set up to carry out complex processing and optimization tasks in radar remote sensing and/or exploration of the earth's surface using at least one quantum computer QC and/or in LIDAR remote sensing and/or in ultrasonic exploration and/or exploration of the water surface and/or the airspace and/or the sea area using the SENS sensors. Such an application can include, for example, observation and/or analysis of military issues. Preferably, one or more device components of one or more drones DR1, DR2, DR3 of the drone swarm and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for quantum computing routines and - To carry out quantum computing methods in the area of radar data processing and/or LIDAR data processing and/or ultrasound data processing. Preferably, one or more device components of the drones DR1, DR2, DR3 of the drone swarm and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for focusing raw sensor data to be carried out. Preferably, one or more device components of the drones DR1, DR2, DR3 of the drone swarm and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or provided for this purpose, methods of radar interferometry and/or To carry out ultrasonic interferometry. Preferably, one or more device components of the drones DR1, DR2, DR3 of the drone swarm and/or the quantum computer system QUSYS and/or the quantum computers QC1, QC2 and possibly the central control unit ZSE are set up and/or intended to generate radar images and/or LIDAR data. To generate and/or evaluate images and/or sonar images and/or images based on the sensor data of the SENS sensors of one or more drones DR1, DR2, DR3 of the drone swarm and/or satellite data and/or other data.

glossary

vehicle

A vehicle within the meaning of the document presented here can also be a motor vehicle, a two-wheeler, a tricycle or a truck, a commercial vehicle, a robot, a transport vehicle, a drone, a robot drone, a missile, a floating body, a diving body , a ship, a submarine, a sea mine, a landmine, a rocket, a projectile, a satellite, a space station, a trailer, a barge, a container, in particular a sea container and/or smartphone and/or a garment and/or a piece of jewelry and/or a wearable quantum computer system and/or a mobile quantum computer system and/or vehicle and/or robot and/or aircraft and/or a cruise missile and/or underwater vehicle and/or surface floating body and/or underwater floating body and/or or a mobile medical device and/or a deployable weapon system and/or battlefield head and/or surface or underwater vehicle and/or projectile and/or other mobile device and/or movable device and/or the like. If the document presented here describes a specific vehicle, the description also includes and claims all other vehicles described above, as long as this makes sense in the relevant context. In particular, all applications to weapons and weapon systems and mobile medical devices, which can typically be relocated at least temporarily, are also included. In the sense of the document presented here, this document interprets the term vehicle very broadly as a “transportable device”, which may, in particular, temporarily have its own drive and/or aids for transport by water and/or on land and/or in the air and/or in space.

horizontal

The adjective “horizontal” is used in this disclosure as part of the name of the device parts and the associated sizes unless expressly stated otherwise. This happens because the quantum bits are numbered consecutively. This allows the columns (vertical) and rows (horizontal) to be better distinguished within two-dimensional quantum bit arrangements. A “horizontal line” is therefore a line within such a two- or one-dimensional arrangement that runs along a line. The assigned current is then referred to, for example, in an analogous manner as “horizontal line current” to give an example of naming a quantity.

Isotopically pure

A material is isotopically pure within the meaning of this disclosure if the concentration of isotopes other than the base isotopes that dominate the material is so low that the technical purpose is combined to an extent sufficient for the production and sale of products with an economically sufficient level Production yield is achieved. This means that interference caused by such isotopic impurities does not interfere with the functionality of the quantum bits, or at most only does so to a sufficiently small extent. In relation to diamond, this means that the diamond preferably consists essentially of ¹² C isotopes as base isotopes that have no magnetic moment.

Vicinity

For example, when this disclosure refers to a “device that is located near the plumb point (LOTP) or at the plumb point (LOTP) for generating a circularly polarized microwave field,” the term proximity is to be understood in this way that this device exerts or can exert an intended effect with its polarized microwave field or otherwise on the quantum dot (NV) located on the plumb line (LOT), which in turn is intended to be so in connection with the disclosure presented here It should be understood that the intended effect allows a procedural step to be carried out in the functional steps for the intended use of a device proposed here.

NP completeness

In computer science, a problem is called NP-complete (complete for the class of problems that can be solved nondeterministically in polynomial time) if it is one of the most difficult problems in the NP class, i.e. it is both in NP and NP-hard is. In colloquial terms, this means that it probably cannot be solved efficiently.

Formally, NP-completeness is only defined for decision problems (possible solutions only “yes” or “no”), while other types of problems are referred to as NP-equivalence (e.g. search problems or optimization problems). In colloquial language, however, this distinction is often not made, so that one generally speaks of “NP-complete problems”, regardless of whether a decision problem is present or not. This is possible because different problem types can be converted into one another (reducible to one another).

• • in der Komplexitätsklasse NP liegt: Ein deterministisch arbeitender Rechner benötigt nur polynomiell viel Zeit, um zu entscheiden, ob eine vorgeschlagene Lösung eines zugehörigen Suchproblems tatsächlich eine Lösung ist, und
• • zu den NP-schweren Problemen gehört: Alle anderen Probleme, deren Lösungen deterministisch in polynomieller Zeit überprüft werden können, können auf das Problem derart zurückgeführt werden, dass diese Rückführung auf einem deterministischen Rechner höchstens polynomielle Zeit in Anspruch nimmt. Man spricht von einer Polynomialzeitreduktion.

A decision problem is NP-complete if it

• • is in the complexity class NP: A deterministic computer only needs a polynomial amount of time to decide whether a proposed solution to an associated search problem is actually a solution, and
• • belongs to the NP-hard problems: All other problems whose solutions can be checked deterministically in polynomial time can be reduced to the problem in such a way that this reduction takes at most polynomial time on a deterministic computer. This is called a polynomial time reduction.

NP-complete problems probably cannot be solved efficiently because solving them on real computers takes a long time. In practice, this does not have a negative effect in every case, that is, for many NP-complete problems there are solution procedures that can be used to solve them in practice occurring orders of magnitude can be solved in an acceptable time.

• • Für kein NP-vollständiges Problem konnte bisher nachgewiesen werden, dass es in polynomieller Zeit lösbar wäre.
• • Falls nur ein einziges dieser Probleme in polynomieller Zeit lösbar wäre, dann wäre jedes Problem in NP in polynomieller Zeit lösbar, was große Bedeutung für die Praxis haben könnte (jedoch nicht notwendigerweise haben muss).

Many important problems that arise in practice are NP-complete, which makes NP-completeness a central concept in computer science. This importance is further reinforced by the so-called P-NP problem:

• • No NP-complete problem has yet been shown to be solvable in polynomial time.
• • If only one of these problems were solvable in polynomial time, then every problem in NP would be solvable in polynomial time, which could (but does not necessarily have) great practical importance.

Since Cook's introduction of NP-completeness, completeness has been expanded into a general concept for arbitrary complexity classes.

PQC (Post Quantum Cryptography)

• „In der Kryptografie bezieht sich die Post-Quantum-Kryptografie (manchmal auch als quantensicher, quantensicher oder quantenresistent bezeichnet) auf kryptografische Algorithmen (in der Regel Public-Key-Algorithmen), von denen man annimmt, dass sie gegen einen kryptoanalytischen Angriff durch einen Quantencomputer sicher sind. Das Problem bei den zur Zeit der Anmeldung dieses Dokuments gängigen Algorithmen ist, dass ihre Sicherheit auf einem von drei schwierigen mathematischen Problemen beruht: dem Problem der ganzzahligen Faktorisierung, dem Problem des diskreten Logarithmus oder dem Problem des diskreten Logarithmus mit elliptischen Kurven. Alle diese Probleme können auf einem ausreichend leistungsfähigen Quantencomputer, auf dem der Shor-Algorithmus läuft, leicht gelöst werden.
• Obwohl die derzeit öffentlich bekannten experimentellen Quantencomputer nicht über die nötige Rechenleistung verfügen, um einen echten kryptografischen Algorithmus zu brechen, entwickeln viele Kryptografen neue Algorithmen, um sich auf eine Zeit vorzubereiten, in der Quantencomputer zu einer Bedrohung werden. Diese Arbeit hat durch die PQCrypto-Konferenzreihe seit 2006 und in jüngerer Zeit durch mehrere Workshops über sichere Quantenkryptografie, die vom Europäischen Institut für Telekommunikationsnormen (ETSI) und dem Institut für Quanteninformatik veranstaltet wurden, größere Aufmerksamkeit bei Wissenschaftlern und Industrie erlangt.
• Im Gegensatz zu der Bedrohung, die die Quanteninformatik für die derzeitigen Public-Key-Algorithmen darstellt, gelten die meisten derzeitigen symmetrischen Verschlüsselungsalgorithmen und Hash-Funktionen als relativ sicher gegenüber Angriffen von Quantencomputern.[2][7] Der Quanten-Grover-Algorithmus beschleunigt zwar Angriffe auf symmetrische Verschlüsselungen, aber eine Verdoppelung der Schlüsselgröße kann diese Angriffe wirksam abwehren.[8] Daher muss sich die symmetrische Post-Quantum-Kryptografie nicht wesentlich von der derzeitigen symmetrischen Kryptografie unterscheiden.”

Quote from Wikipedia:

• “In cryptography, post-quantum cryptography (sometimes referred to as quantum-safe, quantum-proof, or quantum-resistant) refers to cryptographic algorithms (typically public-key algorithms) that are believed to be effective against a cryptanalytic attack by one Quantum computers are safe. The problem with the algorithms in use at the time of filing this document is that their security relies on one of three difficult mathematical problems: the integer factorization problem, the discrete logarithm problem, or the discrete logarithm problem with elliptic curves. All of these problems can be easily solved on a sufficiently powerful quantum computer running Shor's algorithm.
• Although currently publicly known experimental quantum computers do not have the computing power necessary to break a real cryptographic algorithm, many cryptographers are developing new algorithms to prepare for a time when quantum computers become a threat. This work has gained greater academic and industry attention through the PQCrypto conference series since 2006 and more recently through several workshops on secure quantum cryptography organized by the European Telecommunications Standards Institute (ETSI) and the Institute for Quantum Computing.
• In contrast to the threat that quantum computing poses to current public key algorithms, most current symmetric encryption algorithms and hash functions are considered relatively secure against attacks from quantum computers.[2][7] Although the Quantum Grover algorithm accelerates attacks on symmetric encryption, doubling the key size can effectively deter these attacks.[8] Therefore, symmetric post-quantum cryptography need not differ significantly from current symmetric cryptography.”

Quantum computer program and quantum operation and quantum op-code

In the sense of the document presented here, a quantum computer program is a program that includes at least one quantum operation and is executed by a control device µC of a deployable quantum computer QC. One or more binary data in the memory NVN, RAM of the control device μC of the deployable quantum computer QC preferably encode such a quantum operation. For example, it can be a predetermined data word. A quantum operation in the sense of the document presented here manipulates at least the quantum state of at least one quantum dot of the quantum dots NV1, NV2, NV3 of the deployable quantum computer QC and/or manipulates at least the quantum state of at least one core quantum dot of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , CI2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the deployable quantum computer QC. The technical teaching of the document presented here also refers to the data word that symbolizes such a quantum operation as a quantum op code. A quantum computer program therefore includes at least one quantum op-code. The quantum op code can also include multiple data words.

Pure substrate

A pure substrate within the meaning of this disclosure exists when the concentration of atoms other than the base atoms that dominate the material of the substrate is so low that the technical purpose is sufficient for the production and sale of products an economically sufficient production yield is achieved. This means that disruptions caused by such atomic impurities do not disrupt the functionality of the quantum bits, or at most only do so to a sufficiently small extent. In relation to diamond, this means that the diamond preferably consists essentially of carbon atoms and contains no or only an insignificant number of foreign atoms. The substrate preferably contains as little ferro as possible magnetic impurities such as Fe and/or Ni, as their magnetic fields can interact with the spin of the quantum dot (NV).

insignificant phase rotation

An insignificant phase rotation of the state vector of a quantum dot for the purposes of this disclosure is a phase rotation that can be considered insignificant or correctable for operation and functionality. As a first approximation, it can therefore be assumed to be slightly zero.

vertical

The adjective “vertical” is used in this disclosure as part of the name of the device parts and the associated dimensions unless expressly stated otherwise. This happens because the quantum bits are numbered consecutively. This allows the columns (vertical) and rows (horizontal) to be better distinguished within two-dimensional quantum bit arrangements. A “vertical line” is therefore a line within such a two- or one-dimensional arrangement that is routed along a column. The assigned current is then referred to, for example, in an analogous manner as “vertical line current” to give an example of naming a quantity.

List of Scriptures Cited

If, in the context of the nationalization of an international subsequent application, the law of the respective legal system of the state in which the international application of the document presented here is nationalized allows disclosure by reference, the content of the following documents is a full part of the disclosure presented here. ,
CN 103 855 907 B ,
CN 108 831 576 B ,
CN 20 634 1126 U ,
DE 1 240 967 B ,
DE 1 564 070 B1 ,
DE 2 124 465 B2 ,
DE 7 219 216 U ,
DE 69 411 078 T2 ,
DE 19 602 875 A1 ,
DE 19 738 066 A1 ,
DE 19 957 669 A1 ,
DE 19 782 844 538 B1 ,
DE 10 2014 225 346 A1 ,
DE 10 2018 127 394.0 ,
DE 10 2019 130 114.9 ,
DE 10 2019 120 076.8 ,
DE 10 2019 121 137 ,
DE 10 2020 125 189 A1
DE 10 2020 101 784 B3
DE 10 2020 007 977 B4
DE 10 2021 110 964.7
DE 20 2021 101 169 U1
EP 2 874 292 B1 ,
EP 2 986 852 B1 ,
EP 3 007 350 B1 ,
EP 3 075 064 A1 ,
EP 3 093 966 B1 ,
EP 3 279 603 B1 ,
EP 3 345 290 B1 ,
EP 3 400 642 B1 ,
EP 3 646 452 B1 ,
EP 3 863 165 A1 ,
RU 126 229 U1 ,
RU 2 566 620 C2 ,
RU 2014 143 858 A ,
US 5,443,657 A ,
US 5,859,484 A ,
US 8,552,616 B2 ,
US 2016 377 029 A1 ,
US 2018 226 165 A1 ,
US 2019 368 464 A1 ,
US 2021 147 061 A1 ,
WO 2009 103 974 A1 ,
WO 2014 031 037 A2
WO 2016 100 008 A2 ,
WO 2019 143 396 A2 ,
WO 2021 159 117 A1 ,
https://en.wikipedia.org/wiki/Supersingular_isogeny_key_exchange
https://en.wikipedia.org/wiki/Post-quantum_cryptography
https://de.wikipedia.org/wiki/Liste_der_Quantengatter
https://ntrs.nasa.gov/api/citations/20110011201/downloads/20110011201.pdf
https://de.wikipedia.org/wiki/Daisy_Chain
https://en.wikipedia.org/wiki/Cryocooler
https://de.wikipedia.org/wiki/NP-Vollst%C3%A4ndigkeit#: ^~ :text=In%20der%201nformatik%20refers%20man%20a%20problem% 20as, this%20distinction%20but%20often%20not %20completed%2C%20so%20
https://en.wikipedia.org/wiki/NP-hardness
https://ntrs.nasa.gov/api/citations/20110011201/downloads/20110011201.pdf
Book Daniel J. Bernstein, Johannes Buchmann, Erik Dahmen "Post-Quantum Cryptography" November 19, 2008"Springer; 2009. Edition (November 19, 2008), ISBN-10: 3540887016, ISBN-13: 978-3540887010
Ovidiu Calin, “Deep Learning Architectures: A Mathematical Approach (Springer Series in the Data Sciences),” Springer; 1st ed. 2020 Edition (February 14, 2021), ISBN-10: 3030367231, ISBN-13: 978-3030367237
Franklin R. Chang Diaz, F. Wall y Baitty, Jared P. Squire, Richard H. Goulding, Edgar A. Bering, Roger D. Bengtson, “The Vasimr Engine: Project Status and Recent Accomplishments,” downloadable January 9, 2022 from https://ntrs.nasa.gov/api/citations/20110011201/downloads/20110011201.pdf.
Hugo K. Messerle (author), “Magnetohydrodynamic Electrical Power Generation (UNESCO Energy Engineering Series)”, John Wiley & Sons Ltd (August 1, 1995), ISBN-10: 0471942529, ISBN-13: 978-0471942528.
Steven Prawer (Editor), Igor Aharonovich (Editor), “Quantum Information Processing with Diamond: Principles and Applications”, Woodhead Publishing Series in Electronic and Optical Materials, Volume 63, Woodhead Publishing, May 8, 2014, ISBN-10: 0857096567, ISBN-13: 978-0857096562
Petr Siyushev, Milos Nesladek, Emilie Bourgeois, Michal Gulka, Jaroslav Hruby, Takashi Yamamoto, Michael Trupke, Tokuyuki Teraji, Junichi Isoya, FedorJelezko, “Photoelectrical imaging and coherent spin-state readout of single nitrogen-vacancy centers in diamond,” Science 363 , 728-731 (2019) 15 February 2019
Akinori Tanaka, Akio Tomiya, Koji Hashimoto, “Deep Learning and Physics (Mathematical Physics Studies)” February 21, 2021, Publisher: Springer; 1st ed. 2021 Edition, ISBN-10: 9813361077, ISBN-13: 978-9813361072
Vasily Y. Ushakov (author), “Electrical Power Engineering: Current State, Problems and Perspectives (Green Energy and Technology)”, paperback - August 18, 2018, Springer; 1st ed. 2018 Edition (August 18, 2018), ISBN-10: 3319872850, ISBN-13: 978-3319872858.

Reference symbol list

1

Software stack of the proposed quantum computer QC;

2

application program;

3

hybrid quantum technology/classical programs and software;

4

classical algorithms;

5

classic programs and software;

6

classic computer hardware, especially in von Neumann or Harvard architecture;

7

quantum technology algorithms;

8th

abstract quantum gate models;

9

Transcompilers, optimizers and quantum error correction;

10

11

quantum gate hardware model;

12

Control program 12 for the control and control of one or more microwave and/or radio wave frequency generators MW/RF-AWFG for generating an electromagnetic wave field by means of one or more microwave and/or radio wave antennas mWA, in particular vertical lines LV1, LV2 or horizontal lines LH1 at the respective location of the quantum dots NV1, NV2, NV3, to influence the quantum states of the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , CI2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC;

13

SPc laser control program 13 for the control and control of the waveform generator WFG and the light source driver LDRV and thus the light source LD for the generation of light pulses by means of the waveform generator WFG and the light source driver LDRV and the light source LD;

14

Control program 14 for controlling the reading of the quantum states of the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , CI2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC using the control device µC. It is preferably a control program 14 for controlling, monitoring and reading out values of the means PD, V for optically reading out the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots _Cl11 , _Cl12 , Cl1 ₃ , Cl2 ₁ , CI2 ₂ , Cl2 3, Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC by the control device µC and/or a control program 14 for _controlling the control and reading out of values of the means for electrically reading out the quantum dots NV1, NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC;

15

Control program 15 for detecting the magnetic flux density B in the area of the quantum dots _NV1 , NV2, NV3 of the quantum computer QC and/or the quantum states of the core quantum dots Cl11, _Cl12 , _Cl13 , _Cl21 , _CI22 , _Cl23 , _Cl31 , Cl3 ₂ , Cl3 ₃ of the quantum computer QC by means of magnetic field sensors MSx for the magnetic flux density B _x in the direction of the X-axis and/or by means of magnetic field sensors MSy for the magnetic flux density B _y in the direction of the Y-axis and/or by means of magnetic field sensors MSz for the magnetic flux density B _z in the direction of the Z-axis and/or for controlling and controlling magnetic field controls MFSx, MFSy, MFSz and/or for controlling and controlling magnetic field generating means MGx, MGy, MGz;

16

Control program 16 for controlling the optical system OS in order to optimize the irradiation of the laser beam LB into the substrate D if necessary;

17

Control program 17 for execution by the control device µC and for controlling and setting DC current levels and/or DC voltage levels to influence specific quantum points NV1, NV2, NV3 of the quantum computer QC and/or specific core quantum points Cl1 ₁ , Cl1 ₂ , Cl1 ₃ , Cl2 ₁ , CI2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ of the quantum computer QC in such a way that they may not participate in a hardware operation or participate in a hardware operation.;

18

NOT USED,

19

Software part of the software stack;

20

Hardware part of the software stack;

21

inner quantum computer;

22

Position control program 22 for checking and controlling a positioning device XT, YT for positioning and, if necessary, aligning the substrate D with respect to the optical system OS;

23

Temperature control program 23 for controlling one or more cooling devices KV and / or one or more closed loop helium gas cooling systems HeCLCS;

24

Any existing vehicle control program 24 for checking and controlling any existing vehicle functions of a possibly moving, deployable quantum computer QC;

25

possibly used for communication by the control computer µC cryptography program 25 for encrypting and/or decrypting data that the quantum computer QC and/or the control device µC receive or send via the data interface DBIF, and/or for encrypting and/or decrypting other data from the quantum computer QC. It is preferably a PQC-capable cryptography method,

26

one or more measured value acquisition programs 26 for querying the measured values and for controlling and monitoring the associated measuring systems;

27

Vehicle condition determination program 27 for assessing the situation of the overall condition of the vehicle and/or the surroundings of the vehicle depending on measured values;

28

Data interface program. For controlling and controlling one or more data interfaces DBIF;

ADCV

Amplifier V analog-to-digital converter;

AS

Shielding;

BENG

first energy reserve;

BENG2

second energy reserve;

BNV

rotating magnetic field;

BSC

back contact;

BTR

Energy reserve of the vehicle (submarine, motor vehicle, etc.);

CBA

control unit A;

CBB

control unit B;

CECEQUREG

nuclear-electron-nuclear-electron quantum register;

CEQUREG1

first nuclear-electron quantum register;

CEQUREG2

second core-electron quantum register;

Cl1

first nuclear quantum dot. Preferably, the exemplary first core quantum dot Cl1 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the region of the core quantum dot Cl1 preferably comprises essentially or even more preferably absolutely no isotopes with a magnetic nuclear moment. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 .;

Cl11

first core quantum point Cl1 ₁ of the first quantum ALU QUALU1. The exemplary first core quantum dot Cl1 ₁ of the first quantum ALU QUALU1 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot Cl1 ₁ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The first core quantum point Cl1 ₁ of the first quantum ALU QUALU1 is in the 3 not shown for clarity. The reader should assume that in the 3 the first core quantum dot Cl1 ₁ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1 as in the 2 the first core quantum dot Cl1 ₁ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

Cl12

second core quantum point Cl1 ₂ of the first quantum ALU QUALU1. The exemplary second core quantum dot Cl1 ₂ of the first quantum ALU QUALU1 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot Cl1 ₂ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The second core quantum dot Cl1 ₂ of the first quantum ALU QUALU1 is in the 3 not shown for clarity. The reader should assume that in the 3 the second core quantum dot Cl1 ₂ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1 as in the 2 the second core quantum dot Cl1 ₂ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

Cl13

third core quantum dot Cl1 ₃ of the first quantum ALU QUALU1 Preferably, the exemplary third core quantum dot Cl1 ₃ of the first quantum ALU QUALU1 is an isotope with a magnetic nuclear moment in the substrate D, the substrate D in the area of the core quantum dot Cl1 ₃ preferably substantially or still more preferably comprises absolutely no isotopes with a nuclear magnetic moment. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The third core quantum point Cl1 ₃ of the first quantum ALU QUALU1 is in the 3 not shown for clarity. The reader should assume that in the 3 the third core quantum point Cl1 ₃ of the first quantum ALU QUALU1 is coupled to the first quantum point NV1 as in the 2 the third core quantum dot Cl1 ₃ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

C12

second core quantum dot. Preferably, the exemplary second core quantum dot C12 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the region of the core quantum dot CI2 preferably comprises essentially or even more preferably absolutely no isotopes with a magnetic nuclear moment. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 .;

Cl21

first core quantum dot Cl2 ₁ of the second quantum ALU QUALU2. Preferably, the exemplary first core quantum dot Cl2 ₁ of the second quantum ALU QUALU2 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot Cl2 ₁ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The first core quantum dot Cl2 ₁ of the second quantum ALU QUALU2 is in the 3 not shown for clarity. The reader should assume that in the 3 the first core quantum dot Cl2 ₁ of the second quantum ALU QUALU2 is coupled to the second quantum dot NV2 as in the 2 the first core quantum dot Cl2 ₁ of the second quantum ALU QUALU2 is coupled to the second quantum dot NV2;

Cl22

second core quantum dot Cl2 ₂ of the second quantum ALU QUALU2. The exemplary second core quantum dot Cl2 ₂ of the second quantum ALU QUALU2 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot Cl2 ₂ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The second core quantum dot Cl2 ₂ of the second quantum ALU QUALU2 is in the 3 not shown for clarity. The reader should assume that in the 3 the second core quantum dot Cl2 ₂ of the second quantum ALU QUALU2 is coupled to the second quantum dot NV2 as in the 2 the second core quantum dot Cl2 ₂ of the second quantum ALU QUALU2 is coupled to the second quantum dot NV2;

Cl23

third core quantum point C12 ₃ of the second quantum ALU QUALU2. The exemplary first core quantum dot C12 ₃ of the second quantum ALU QUALU2 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot Cl2 ₃ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The third core quantum dot Cl2 ₃ of the second quantum ALU QUALU2 is in the 3 not shown for clarity. The reader should assume that in the 3 the third core quantum point Cl2 ₃ of the second quantum ALU QUALU2 is coupled to the second quantum point NV2 as in the 2 the third core quantum dot Cl2 ₃ of the second quantum ALU QUALU2 is coupled to the second quantum dot NV2;

CI3

third core quantum dot. Preferably, the exemplary third core quantum dot CI3 is an isotope with a nuclear magnetic moment in the substrate D, wherein the substrate D in the region of the core quantum dot Cl3 preferably comprises essentially or even more preferably absolutely no isotopes with a nuclear magnetic moment. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 ;

Cl31

first core quantum point Cl3 ₁ of the third quantum ALU QUALU3. The exemplary first core quantum dot Cl3 ₁ of the third quantum ALU QUALU3 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot Cl3 ₁ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The first core quantum dot Cl3 ₁ of the third quantum ALU QUALU3 is in the 3 and in the 2 not shown for clarity. The reader should assume that in the 3 the first core quantum point Cl3 ₁ of the third quantum ALU QUALU3 is coupled to the third quantum point NV3 as in the 2 the first core quantum dot Cl1 ₁ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

CI32

second core quantum point Cl3 ₂ of the third quantum ALU QUALU3. The exemplary second core quantum dot Cl3 ₂ of the third quantum ALU QUALU3 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot Cl3 ₂ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The second core quantum point Cl3 ₂ of the third quantum ALU QUALU3 is in the 3 and in the 2 not shown for clarity. The reader should assume that in the 3 the second core quantum dot Cl3 ₂ of the third quantum ALU QUALU3 is coupled to the third quantum dot NV3 as in the 2 the second core quantum dot Cl1 ₂ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

Cl33

third core quantum point Cl3 ₃ of the third quantum ALU QUALU3. The exemplary first core quantum dot Cl3 ₃ of the third quantum ALU QUALU3 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot Cl3 ₃ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The third core quantum point Cl3 ₃ of the third quantum ALU QUALU3 is in the 3 and in the 2 not shown for clarity. The reader should assume that in the 3 the third core quantum point Cl3 ₃ of the third quantum ALU QUALU3 is coupled to the third quantum point NV3 as in the 2 the first core quantum dot Cl1 ₁ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

CIF

first camera interface;

ClF2

second camera interface;

CM1

first camera;

CM2

second camera;

CPU

computer core;

D

substrate;

d1

first distance at which the first quantum dot NV1 is located below the surface OF of the substrate D;

d2

second distance at which the second quantum dot NV2 is located below the surface OF of the substrate D;

DBIF

data interface;

DBIFa

Data interface A;

DBlFb

data interface B;

DBS

dichroic mirror;

DEV

Energy supply of other device parts of the quantum computer QC, which typically also concerns device parts with other reference numbers. For a better overview, the power supply lines of the remaining device parts of the quantum computer QC are shown in the 1 not shown;

DR1

first drone;

DR2

second drone;

DR3

third drone;

CLOSELY

propulsion of the vehicle;

ERS

energy system;

EXDB

external data bus;

EV

Power supply;

λfl

fluorescent radiation wavelength;

λpmp.

pump radiation wavelength;

FHB

factory hall or stationary device;

fHR

microwave and/or radio wave frequency;

FL

fluorescent radiation;

FLC

Fire control station. The fire control center can be a central control unit ZSE.

FLR

attitude control system;

FZ

Airplane;

FZT

aircraft carriers;

GDX

X control device for the translational positioning device in the X direction XT;

GDY

Y control device for the translational positioning device in the Y direction YT;

GH

Housing;

GPS

Navigation system or device for determining the position and/or orientation of the quantum computer QC. If necessary, the navigation system can also determine translational speeds and/or rotational speeds of the quantum computer QC and report them to the computer core CPU of the control device µC of the quantum computer QC via the internal data bus INTDB. If necessary, the navigation system can also determine translational accelerations and/or rotational accelerations of the quantum computer QC and report them to the computer core CPU of the control device µC of the quantum computer QC via the internal data bus INTDB;

HD1

first horizontal driver stage for controlling the first quantum dot NV1 to be controlled;

HD2

second horizontal driver stage for controlling the second quantum dot NV2 to be controlled;

HD3

third horizontal driver stage for driving the third quantum dot NV3 to be controlled;

HeCLCS

Closed Loop Helium Gas Cooling System;

HS1

first horizontal receiver stage HS1, which can form a unit with the first horizontal driver stage HD1, for controlling the first quantum dot NV1 to be controlled;

HS2

second horizontal receiver stage HS2, which can form a unit with the second horizontal driver stage HD2, for controlling the second quantum dot NV2 to be controlled;

HS3

third horizontal receiver stage HS3, which can form a unit with the third horizontal driver stage HD3, for controlling the third quantum dot NV3 to be controlled;

lH1

first horizontal stream. The first horizontal current is the electrical current that flows through the first horizontal line LH1.

IH2

second horizontal stream. The second horizontal current is the electrical current that flows through the second horizontal line LH2.

IH3

third horizontal stream. The third horizontal current is the electrical current that flows through the third horizontal line LH3.

lp

Intensity of the pulses of the pulsed pump radiation LB from the light source LD;

lpHF

Amplitude l _pHF of a pulse of the time envelope curve of the radiation of an electromagnetic field by the one or more devices MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots Cl1 ₁ Cl1 ₂ , Cl1 ₃ , Cl2 ₁ Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ ;

IS

Isolation;

ISH1

first horizontal shield current flowing through the first horizontal shield line SH1;

ISH2

second horizontal shield current current flowing through the second horizontal shield line SH2;

ISH3

third horizontal shield current current flowing through the third horizontal shield line SH3;

ISH4

fourth horizontal shield current current flowing through the fourth horizontal shield line SH4;

ISV1

first vertical shield current flowing through the first vertical shield line SV1;

ISV2

second vertical shield current flowing through the second vertical shield line SV2;

IV1

first vertical stream. The first vertical current is the electric current flowing through the first vertical line LV1;

IVV

internal amplifier within amplifier V;

automobile

Car as an example of a vehicle;

KH1

first horizontal contact of the first quantum bit QUB1 with the first quantum dot NV1. The first horizontal contact of the first quantum bit QUB1, for example, electrically connects the first horizontal shielding line SH1 in the first quantum bit QUB1 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KH2

second horizontal contact of the first quantum bit QUB1 with the first quantum dot NV1 and first horizontal contact of the second quantum bit QUB2 with the second quantum dot NV2. The first quantum bit QUB1 and the second quantum bit QUB2 use the in the example 3 this contact together. The contact, for example, electrically connects the second horizontal shielding line SH2 in the first quantum bit QUB1 and in the second quantum bit QUB2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KH3

second horizontal contact of the second quantum bit QUB2 with the second quantum dot NV2 and first horizontal contact of the third quantum bit QUB3 with the third quantum dot NV3. The second quantum bit QUB2 and the third quantum bit QUB3 use the in the example 3 this contact together. The contact, for example, electrically connects the third horizontal shielding line SH3 in the second quantum bit QUB2 and in the third quantum bit QUB3 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KH4

second horizontal contact of the third quantum bit QUB3 with the third quantum dot NV3. The contact, for example, electrically connects the fourth horizontal shielding line SH3 in the third quantum bit QUB3 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV11

first vertical contact of the first quantum bit QUB1 with the first quantum dot NV1. The first vertical contact of the first quantum bit QUB1 electrically connects the first vertical shielding line SV1 in the first quantum bit QUB1 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV12

second vertical contact of the first quantum bit QUB1 with the first quantum dot NV1. The second vertical contact of the first quantum bit QUB1 preferably electrically connects the second vertical shielding line SH2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV21

first vertical contact of the second quantum bit QUB2 with the second quantum dot NV2. The first vertical contact of the second quantum bit QUB2 electrically connects the first vertical shielding line SV1 in the second quantum bit QUB2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV22

second vertical contact of the second quantum bit QUB2 with the second quantum dot NV2. The second vertical contact of the second quantum bit QUB2 preferably electrically connects the second vertical shielding line SH2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV31

first vertical contact of the third quantum bit QUB3 with the third quantum dot NV3. The first vertical contact of the third quantum bit QUB3 electrically connects the first vertical shielding line SV1 in the third quantum bit QUB3 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV32

second vertical contact of the third quantum bit QUB3 with the third quantum dot NV3. The second vertical contact of the third quantum bit QUB3 preferably electrically connects the second vertical shielding line SH2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV

relocatable cooler;

L.B

pump radiation;

LD

light source;

LDRV

light source driver;

LDV

loading device;

LH1

first horizontal line;

LH2

second horizontal line;

LH3

third horizontal line;

LM

Lamp with a light source;

LV1

first vertical line;

µC

control device;

µC1

first control device of the first quantum computer QC1;

µC1a

first control device A of the first quantum computer QC1;

µC1b

first control device B of the first quantum computer QC1;

pC2

second control device of the second quantum computer QC2;

µC3

third control device of the third quantum computer QC3;

pC4

fourth control device of the fourth quantum computer QC4;

µC5

fifth control device of the fifth quantum computer QC5;

µC6

sixth control device of the sixth quantum computer QC6;

µC7

seventh control device of the seventh quantum computer QC7;

µC8

eighth control device of the eighth quantum computer QC8;

µC9

ninth control device of the ninth quantum computer QC9;

µC10

tenth control device of the tenth quantum computer QC10;

µC11

eleventh control device of the eleventh quantum computer QC11;

µC12

twelfth control device of the twelfth quantum computer QC12;

µC13

thirteenth control device of the thirteenth quantum computer QC13;

µC14

fourteenth control device of the fourteenth quantum computer QC14;

µC15

fifteenth control device of the fifteenth quantum computer QC15;

µC16

sixteenth control device of the sixteenth quantum computer QC16;

µCV

Amplifier V control device;

MDBIF

internal data interface MDBIF;

MEMDBV

Memory data bus between control device µCV of amplifier V and memory MEMV of amplifier V;

MEMV

Amplifier V memory;

MFSx

first magnetic field control;

MFSy

second magnetic field control;

MFSz

third magnetic field control;

MGx

first magnetic field generating means, which preferably generates a magnetic flux density B _x , which preferably essentially has a direction which preferably corresponds to the first direction, for example the direction of the X axis;

MGy

second magnetic field generating means, which preferably generates a magnetic flux density B _y , which preferably essentially has a direction which preferably corresponds to the second direction, for example the direction of the Y axis;

MGz

third magnetic field generating means, which preferably generates a magnetic flux density B _z , which preferably essentially has a direction which preferably corresponds to the third direction, for example the direction of the Y axis;

MSx

Magnetic field sensor for the magnetic flux density B _x in the direction of the X axis;

MSy

Magnetic field sensor for the magnetic flux density B _y in the direction of the Y axis;

MSz

Magnetic field sensor for the magnetic flux density B _z in the direction of the Z axis;

mWA

microwave and/or radio wave antenna;

MW/RF AWFG

Microwave and/or radio wave frequency generator for generating largely freely definable waveforms (English: arbitrary wave form generator);

NAV

navigation system and/or autopilot;

NV1

first quantum dot. Preferably, the exemplary first quantum dot NV1 is a paramagnetic center in the substrate D. Preferably, the exemplary first quantum dot NV1 is an NV center or a SiV center or an ST1 center in the substrate D;

NV2

second quantum dot. Preferably, the exemplary second quantum dot NV2 is a paramagnetic center in the substrate D. Preferably, the exemplary second quantum dot NV2 is an NV center or a SiV center or an ST1 center in the substrate D;

NV3

third quantum dot. Preferably, the exemplary third quantum dot NV3 is a paramagnetic center in the substrate D. Preferably, the exemplary third quantum dot NV3 is an NV center or a SiV center or an ST1 center in the substrate D;

NVM

non-volatile memory;

OF

Surface;

O.S

optical system;

OSZ

Clock of the computer core CPU of the control device µC of the quantum computer QC;

P.D

photodetector;

PM

permanent magnet;

PV

Positioning device for the permanent magnet PM;

PVC

Control device for the positioning device PV for the permanent magnet PM;

PWR

Energy supply to the charging device LDV;

QC

quantum computers;

QC1

first quantum computer;

QC2

second quantum computer;

QC3

third quantum computer;

QC4

fourth quantum computer;

QC5

fifth quantum computer;

QC6

sixth quantum computer;

QC7

seventh quantum computer;

QC8

eighth quantum computer;

QC9

ninth quantum computer;

QC10

tenth quantum computer;

QC11

eleventh quantum computer;

QC12

twelfth quantum computer;

QC13

thirteenth quantum computer;

QC14

fourteenth quantum computer;

QC15

fifteenth quantum computer;

QC16

sixteenth quantum computer;

QCTV

Quantum computer system separation device. The quantum computer system separation device preferably separates an external data bus EXTDB, which, for example, connects a first quantum computer system QUSYS with a second quantum computer system QUSYS, if necessary, so that the quantum computer system QUSYS, which previously included the first and the second quantum computer system QUSYS, breaks down into two separate quantum computer systems QUSYS due to the separation. However, the quantum computer system separation device can also connect a previously separate first quantum computer system QUSYS with a previously separate second quantum computer system QUSYS and, if necessary, couple them, so that the quantum computer system QUSYS is created, which then comprises the first and second quantum computer systems QUSYS by connecting these two quantum computer systems via quantum computer system separation device into one Quantum computer system QUSYS merges;

QUALU1

first quantum ALU. The exemplary first quantum ALU consists of a first quantum point NV1 and a first core quantum point Cl1 ₁ of the first quantum ALU and a second core quantum point Cl1 ₂ of the first quantum ALU and a third core quantum point Cl1 ₃ of the first quantum ALU ( 2 );

QUALU2

second quantum ALU. The exemplary second quantum ALU consists of a second quantum point NV2 and a first core quantum point Cl2 ₁ of the second quantum ALU and a second core quantum point Cl2 ₂ of the second quantum ALU and a third core quantum point C12 ₃ of the second quantum ALU ( 2 );

QUSYS

deployable quantum computing system;

R.A.M.

volatile memory;

RKT

Rocket. The rocket is just an example of a possible payload. The payload itself can include one or more QUSYS quantum computer systems. Preferably, the quantum computer system QUSYS of the payload is connected to the quantum computer system QUSYS of the vehicle FZ, or the object in which the payload is set up or stored, for example via an external data bus EXTDB during the time of the payload;

RKTC

missile launch control;

50

receiver output signal;

S1

reception signal;

S4

measured value signal;

S5

broadcast signal;

SC

Sea containers. The sea container is just one example of a transportable container in which one or more QUSYS quantum computer systems or one or more QC quantum computers can be operated;

SCHR

ship propeller;

SDB

control data bus;

SDBV

internal control data bus within the amplifier V;

SENS

one or more sensors;

SH1

first horizontal shield line;

SH2

second horizontal shield line;

SH3

third horizontal shield line;

SH4

fourth horizontal shield line;

SRG

first energy processing device, in particular a voltage converter or a voltage regulator or a current regulator;

SRG2

second energy processing device, in particular a voltage converter or a voltage regulator or a current regulator;

ST

temperature sensor;

STM

semi-transparent mirror;

SUB

submarine;

SV1

first horizontal shield line;

SV2

second vertical shield line;

TL

Low loader. The low loader is an example of a vehicle without its own propulsion.

TRP

torpedoes;

TRPC

torpedo launch control;

T.S

separator;

t0HF

Reference time of a pulse of the pulsed electromagnetic field with microwave and/or radio wave frequency f _HF . Preferably, the reference time t _0HF is equal to the reference time t _op for a pulse sequence or at a fixed time interval from the reference time for a pulse sequence t _0p ;

t0p

Reference time for a pulse sequence. Preferably, the reference time t _0p for a pulse sequence is equal to the reference time t _0HF or at a fixed time interval from the reference time t _0HF ;

tdp

the time duration t _dp of the pulses of the pulsed pump radiation LB of the light source LD;

tdHF

temporal pulse duration of the pulse of the pulsed electromagnetic field with microwave and/or radio wave frequency f _HF . It is the temporal pulse duration of the temporal envelope curve of the radiation of an electromagnetic field by the one or more devices MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots Cl1 ₁ Cl1 ₂ , Cl1 ₃ , Cl2 ₁ Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ in pulse form;

tsp

Temporal position of the pulses of the pulsed pump radiation LB of the light source LD relative to a reference time t ₀ As a rule, the temporal position t _sp of a pulse denotes the starting time of the relevant pulse;

tspHF

Pulse start time t _spHF relative to the reference time t _0HF of a pulse of the temporal envelope curve of the radiation of an electromagnetic field by the one or more devices MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots Cl1 ₁ Cl1 ₂ , Cl1 ₃ , Cl2 ₁ Cl2 ₂ , Cl2 ₃ , Cl3 ₁ , Cl3 ₂ , Cl3 ₃ ;

UDB1

first sub-data bus;

UDB2

second sub-data bus;

UDB3

third sub-data bus;

UDB4

fourth sub-data bus;

ÜOSZ

Monitoring clock generation of the quantum computer monitoring device QUV of the quantum computer QC;

US

bottom of substrate D;

v

Amplifier;

V1

Output signal of the internal amplifier IVV of the amplifier V and input signal of the analog-to-digital converter ADCV of the amplifier V;

V2

Data line between the control device µCV of the amplifier V and the analog-to-digital converter ADCV of the amplifier V;

Vbatext

electrical energy from an external power supply, for example an external power supply;

VD1

first vertical driver stage for controlling the quantum dots NV1, NV2, NV3 to be controlled;

VIF

Data interface of the amplifier V to the control data bus SDB;

VS1

first vertical receiver stage, which can form a unit with the first vertical driver stage VD1, for controlling the first quantum dots NV1, NV2, NV3 to be controlled;

WFG

waveform generator;

XT

translational positioning device in the X direction;

YT

translational positioning device in Y direction;

ZM

Tractor. The tractor is an example of a drive for a container with one or more quantum computers QC and/or one or more quantum computer systems QUSYS, which can be separated from the container or added to the container. In the example of the 6b the container is an exemplary low-loader TL with a sea container SC;

ZSE

central control unit;

QUOTES INCLUDED IN THE DESCRIPTION

This list of documents listed by the applicant was generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.

Cited patent literature

• DE 102021112917 [0001]
• DE 102022105465 [0001]
• DE 102020007977 B4 [0002, 0016, 0206, 0502]
• DE 102020125189 A1 [0002, 0113, 0117, 0124, 0125, 0126, 0140, 0271, 0502]
• DE 102020101784 B3 [0002, 0011, 0502]
• DE 102020125169 A1 [0006, 0010, 0290, 0292, 0293]
• WO 2021083448 A1 [0010]
• DE 102021110964 [0200, 0502]
• DE 202021101169 U1 [0254, 0502]
• WO 2021159117 A1 [0254, 0502]
• EP 3863165 A1 [0254, 0502]
• US 2021147061 A1 [0254, 0502]
• CN 108831576 B [0254, 0502]
• US 2019368464 A1 [0254, 0502]
• WO 2019143396 A2 [0254, 0502]
• EP 3646452 B1 [0254, 0502]
• CN 206341126 U [0254, 0502]
• EP 3279603 B1 [0254, 0502]
• EP 3400642 B1 [0254, 0502]
• EP 3345290 B1 [0254, 0502]
• EP 3093966 B1 [0254, 0502]
• WO 2016100008 A2 [0254, 0502]
• DE 102014225346 A1 [0254, 0502]
• RU 2014143858 A [0254, 0502]
• EP 3007350 B1 [0254, 0502]
• US 2016377029 A1 [0254, 0502]
• RU 2566620 C2 [0254, 0502]
• EP 3075064 A1 [0254, 0502]
• EP 2874292 B1 [0254, 0502]
• EP 2986852 B1 [0254, 0502]
• CN 103855907 B [0254, 0502]
• RU 126229 U1 [0254, 0502]
• WO 2014031037 A2 [0254, 0502]
• DE 1240967 B [0257, 0502]
• DE 1564070 B1 [0257, 0502]
• DE 2124465 B2 [0257, 0502]
• DE 7219216 U [0257, 0502]
• DE 19782844538 B1 [0257, 0502]
• DE 69411078 T2 [0257, 0502]
• US 5443657 A [0257, 0502]
• US 5859484 A [0257, 0502]
• DE 19602875 A1 [0257, 0502]
• DE 19738066 A1 [0257, 0502]
• DE 19957669 A1 [0257, 0502]
• US 8552616 B2 [0257, 0502]
• WO 2009103974 A1 [0257, 0502]
• US 2018226165 A1 [0257, 0502]
• DE 102018127394 [0348, 0502]
• DE 102019130114 [0348, 0502]
• DE 102019120076 [0348, 0502]
• DE 102019121137 [0348, 0502]
• WO 2020239172 A1 [0461, 0468]

Claims (10)

mobile device, wherein the mobile device comprises a quantum computing system (QUSYS) and wherein the quantum computer system (QUSYS) comprises at least one quantum computer (QC1, QC2) and wherein the mobile device comprises sensors (SENS) and these sensors in particular can include and wherein the mobile device comprises sensors (SENS) and/or measuring means and wherein the sensors (SENS) and/or measuring means provide measured values in particular about the environment of the mobile device and/or about states of the mobile device and/or about states of occupants of the mobile device and/or about users of the mobile device and/or about Deliver states of the payload of the mobile device to the quantum computing system (QUSYS) and wherein at least one or more sensors (SENS) of the mobile device is one of the following sensors (SENS) providing measured values or comprises at least one of the following sensors (SENS) providing measured values as a subsystem: - a radar sensor and/or - a microphone and/or - an ultrasound microphone and/or - an infrasonic microphone and/or - an ultrasound transducer and/or - an infrared sensor and/or - a gas sensor and/or - an acceleration sensor and/or - a speed sensor and/or - a radiation detector and/or - an imaging system and/or - a camera and/or - an infrared camera and/or - a multispectral camera and/or - a LIDAR system and/or - an ultrasound measuring system and/or - a Doppler radar system and/or - a quantum radar system and/or - a quantum sensor and/or - a position sensor and/or - a navigation system and/or - a GPS sensor (or a functionally equivalent device) and/or - a position sensor and/or - a particle counter and/or - a detection system for biological substances, in particular for biological agents, and/or - a gravimeter and/or - a compass and/or - a gyroscope and/or - a MEMS sensor and/or - a pressure sensor and/or - an inclination angle sensor and/or - a temperature sensor and/or - a humidity sensor and/or - a wind speed sensor and/or - a wavefront sensor and/or - a microfluidic measuring system and/or - a distance measuring system and/or - a length measuring system and/or - a biological sensor for detecting biological markers and/or viruses and/or microbes or the like and/or - a sensor system for recording biological measured values of vehicle occupants and/or for recording biological measured values of living cargo, in particular of animals and/or biological materials and/or - a seat occupation measurement system and/or - a voltage sensor and/or a current sensor and/or a power sensor - a radar sensor and/or - a LIDAR sensor and/or - an ultrasonic sensor and/or - a camera based sensor and/or - a quantum sensor and/or - a sonar sensor and wherein the quantum computer QC, depending on these measured values, makes a situation assessment for the overall state of the mobile device and / or the environment of the mobile device and / or the states of the mobile device and / or the states of vehicle occupants and / or users / Users of the mobile device and / or the status of the payload of the mobile device is determined. Mobile device according to Claim 1 , wherein the quantum computer QC controls the mobile device and/or device parts of the mobile device as a function of these measured values and/or influences a control of the mobile device or a device part of the mobile device. Mobile device, especially after Claim 1 or 2 , wherein the mobile device comprises a quantum computer system (QUSYS) and wherein the quantum computer system (QUSYS) comprises at least one quantum computer (QC1, QC2) and wherein the mobile device comprises sensors (SENS) and these sensors in particular - radar sensors and / or - lidar sensors and /or - ultrasonic sensors and/or - camera-based sensors and/or - quantum sensors and/or - sonar sensors and wherein the sensors (SENS) transmit sensor data to the quantum computer system (QUSYS). wherein the quantum computer system (QUSYS) is set up to execute one or more quantum algorithms which increase the performance of sensors (SENS) and/or which accelerate the processing of the data and the sensor data of the sensors (SENS) and/or other data. Mobile device according to one of the Claims 1 until 3 , wherein the mobile device is set up to perform processing and optimization tasks in sensor remote sensing and/or exploration of the earth's surface and/or in sonar exploration and/or in ultrasonic exploration using at least one quantum computer (QC1, QC2) of its quantum computer system (QUSYS). /or in image recognition and/or in image processing and/or the exploration of the water surface and/or in the exploration of a marine volume and/or the airspace and/or the sea area using the sensors (SENS). Mobile device according to one of the Claims 1 until 4 , wherein the mobile device is set up to use at least one quantum computer (QC1, QC2) of its quantum computer system (QUSYS) to implement quantum computing routines and/or quantum computing methods in the area of radar data processing and/or sonar data processing and/or ultrasound data processing and/or to carry out LIDAR data processing. Mobile device according to one of the Claims 1 until 5 , wherein the mobile device is set up to focus sensor raw data using at least one quantum computer (QC1, QC2) of its quantum computer system (QUSYS). Mobile device according to one of the Claims 1 until 6 , wherein the mobile device is set up to carry out radar interferometry and/or sonar interferometry methods using at least one quantum computer (QC1, QC2) of its quantum computer system (QUSYS). Mobile device according to one of the Claims 1 until 7 , wherein the vehicle is set up to generate radar images and/or LIDAR images and/or sonar images and/or images based on the sensor data of the sensors (SENS) and/or using at least one quantum computer (QC1, QC2) of its quantum computer system (QUSYS). to generate and/or evaluate satellite data and/or other data. Mobile device according to one of the preceding claims, wherein the mobile device is part of a swarm of mobile devices. Mobile device according to one of the preceding claims, wherein the mobile device - a floating body and / or - a robot and / or - a land vehicle and / or - a vehicle and / or - a motor vehicle and / or - a two-wheeler and / or - a Tricycle and/or - a truck and/or - a commercial vehicle and/or - a transport vehicle and/or - a drone and/or - a robot drone and/or - a missile and/or - a floating body and/or - a ship drone and /or - a diving body and/or - a ship and/or - a submarine and/or - a submarine drone and/or - a torpedo and/or - a sea mine and/or - a land mine and /or - a rocket and/or - a projectile and/or - a satellite and/or - a space station and/or - a spacecraft and/or - a trailer and/or - a barge and/or - a container, in particular a Sea container, and/or - a smartphone and/or - a piece of clothing and/or - a piece of jewelry and/or - a portable quantum computer system (QUSYS) and/or - a mobile quantum computer system (QUSYS) and/or - a vehicle and/ or - a robot and/or - an aircraft and/or - a spacecraft and/or - an underwater vehicle and/or - a surface floating body and/or - an underwater floating body and/or - a mobile medical device and/or - a deployable weapon system and /or - a warhead and/or - a surface or underwater vehicle and/or - a projectile and/or - a weapon system and/or - a gun and/or - an ammunition component and/or - another mobile device and/or - a movable device or such a device includes.

Images